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Spacecraft charging potential during electron-beam injections into space plasmasInjections of nonrelativistic electron beams from an infinite conductor have been simulated by using a two-dimensional electrostatic particle code to study the spacecraft charging potential. The simulations show that the conductor charging potential at the end of simulations does not vary with the beam density when the beam density exceeds four times the ambient density. The reflection coefficient, which determines a percentage of incident electrons reflected by the conductor, increases the charging potential. To charge the conductor to the beam energy, the reflection coefficient needs to be about 0.5. The results are applied to explain the spacecraft charging potential measured during the Sepac experiments on Spacelab 1.
Document ID
19890054340
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Lin, Chin S.
(Southwest Research Inst. San Antonio, TX, United States)
Koga, James
(Southwest Research Institute San Antonio, TX, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1989
Publication Information
Publication: IEEE Transactions on Plasma Science
Volume: 17
ISSN: 0093-3813
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89A41711
Funding Number(s)
CONTRACT_GRANT: F19628-85-K-0004
CONTRACT_GRANT: NAS8-32488
Distribution Limits
Public
Copyright
Other

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