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Use of charging control guidelines for geosynchronous satellite design studiesSeveral of the principle guidelines from the Spacecraft Charging Design Guidelines Handbook are presented with illustrative examples. Use of the geomagnetic substorm specification to qualify satellite designs, the evaluation of satellite designs by using analytical modelling techniques, the use of selected materials and coatings to minimize charging, the tying of all conducting elements to a common ground, and the use of electrical filtering to protect circuits from discharge induced upsets are discussed. Discharge criteria and SCATHA data are excluded.
Document ID
19820006390
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Steves, N. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1980
Publication Information
Publication: Spacecraft Charging Technol., 1980
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82N14263
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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