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Charging and discharging characteristics of a rigid solar arrayTwo rigid solar array panels were subjected to a simulated geosynchronous orbit substorm environment. During the charging sequence, distributions of accumulated surface charge were measured under eclipse and sunlight conditions. Discharge events were characterized with respect to voltage pulse signatures and amplitudes on the solar array bus leads. Post-exposure analysis of the solar array panels indicated that the electrical characteristics were not degraded in spite of the substantial discharge actvity. However, significant cratering and discoloration of the Tedlar dielectric were observed.
Document ID
19820006356
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brady, G. F., Jr.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Vance, D. A.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Greenberg, S. A.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1981
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Charging Technol., 1980
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82N14229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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