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Spacecraft charging modeling development and validation studyThe effects of spacecraft charging are presented. Analytical models of the magnetospheric environment are used to show the charging interaction between the spacecraft and the plasma sheath, the discharge phenomena, and electromagnetic coupling from the discharge to spacecraft components. Ground tests to validate the models are described.
Document ID
19790015880
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Odonnell, E. E.
(Science Applications, Inc. La Jolla, CA, 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
79N24051
Funding Number(s)
CONTRACT_GRANT: F04701-77-C-0166
CONTRACT_GRANT: NAS3-21048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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