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ATS-5 and ATS-6 potentials during eclipseThe ATS 5 and ATS 6 data for spacecraft charging during eclipse conditions is analyzed. The ATS 5 and ATS 6 charged to voltages greater than 100 volts for about 55 percent of the eclipse periods examined. The mean spacecraft potential during eclipse was 2 keV for ATS 5, and the highest potential measured was 10 kilovolts. For ATS 6, the mean potential during eclipse was 4 keV, the highest potential measured 20 keV. The average measured spacecraft potentials for both ATS 5 and 6 depend approximately linearly upon Kp. This relationship is due mainly to the dependence of electron current density on Kp near midnight. Spacecraft potentials at geosynchronous orbit may, to a rough approximation, thus be inferred from ground-based measurements of Kp, the planetary 3-hour index.
Document ID
19790015834
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rubin, A. G.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Garrett, H. B.
(Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Lewis Res. Center Spacecraft Charging Technol., 1978
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
79N24005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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