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Worst case earth charging environmentThe Applications Technology Satellite-6 (ATS-6) geosynchronous satellite charged up to -2200 V in sunlight on day 178, 1974. This event, being the highest known spacecraft charging event in sunlight, is used to estimate a worst case geosynchronous plasma environment for predicting the spacecraft potential in eclipse. The advantage of using this sunlight spectrum as opposed to an eclipse case is that the ion and electron fluxes to the detectors are shifted only slightly due to the spacecraft potential. After correcting the available data for satellite potential and missing data above 81 KeV, it is found that the plasma can be characterized by a single Maxwellian approximation having an electron density of 1.22/cu cm, electron temperature of 16 KeV, hydrogen ion density of 0.24/cu cm, and hydrogen ion temperature of 29 KeV. In eclipse the spacecraft would have charged up to -28 kV, the highest estimated potential to date in the earth's plasma environment.
Document ID
19820057611
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Deutsch, M.-J. C.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1982
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 19
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82A41146
Distribution Limits
Public
Copyright
Other

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