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System aspects of spacecraft chargingSatellites come in a variety of sizes and configurations including spinning satellites and three-axis stabilized satellites. All of these characteristics have a significant effect on spacecraft charging considerations. There are, however, certain fundamentals which can be considered which indicate the nature and extent of the problem. The global positioning system satellite serves to illustrate certain characteristics.
Document ID
19780002228
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bower, S. P.
(Aerospace Corp. El Segundo, CA, United States)
Date Acquired
August 9, 2013
Publication Date
February 24, 1977
Publication Information
Publication: NASA. Lewis Res. Center Proc. of the Spacecraft Charging Technol. Conf.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
78N10171
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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