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Exospheric density measurements from the drag-free satellite TriadThe Triad satellite is maintained within 1 mm of its proof mass (a small metal ball) in a purely gravitational orbit, using a drag-free control system, named Discos, as the disturbance compensation system. The Discos proof mass is surrounded by an outer shell which holds fuel tanks and cold gas jets. The shell shields the proof mass from such nongravitational forces as radiation pressure, atmospheric drag, and micrometeorite impact. Whenever these forces displace the outer shell relative to the proof mass, an error signal is generated by a capacitive bridge sensor, and the satellite is propelled by gas jets to remain centered on the proof mass when the error reaches 1 mm. Local atmospheric densities near 800 km were measured, using ball position data, and the observed accelerations were corrected for the effects of solar radiation pressure. The measured densities reveal a greater dependence on latitude than that indicated by balloon satellites, and also a dependence on longitude. Only a small dependence on Kp, however, was observed in the region where the measurements were made.
Document ID
19760059712
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Moe, K.
(California Univ. Irvine, CA, United States)
Debra, D. B.
(California Univ. Irvine, CA, United States)
Van Patten, R. A.
(Stanford University Stanford, Calif., United States)
Moe, M. M.
(California Univ. Irvine, CA, United States)
Oelker, G.
(California Univ. Irvine, CA, United States)
Ruggera, M. B., Jr.
(California, University Irvine, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: Journal of Geophysical Research
Volume: 81
Subject Category
Geophysics
Accession Number
76A42678
Funding Number(s)
CONTRACT_GRANT: F44620-72-C-0084
Distribution Limits
Public
Copyright
Other

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