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Potentials on large spacecraft in LEOA system-oriented computer code is used to predict surface charging due to voltages generated within a satellite operating in the typical dense plasma environment of LEO. The use of this code is demonstrated by predicting the expansion of electric fields onto a kapton surface from a pinhole over a biased conductor in a LEO environment. The results are compared to a more-exact solution and experimental data.
Document ID
19830036271
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mandell, M. J.
Katz, I.
Cooke, D. L.
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
83A17489
Funding Number(s)
CONTRACT_GRANT: NAS3-22826
Distribution Limits
Public
Copyright
Other

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