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Auroral interactions with ISSADue to its high inclination orbit, International Space Station Alpha (ISSA) will occasionally experience surface charging by the high energy electrons of the auroral environment. This study looks at the frequency of these occurrences and recapitulates a charging model. ISSA should expect about 80 auoral encounters annually. If the plasma contactor is not run continuously, the vehicle may charge several hundred volts. Charge storage on standard space station coatings should not be a problem, but care must be taken that materials are not introduced inadvertently that cannot bleed off accumulated charge in a reasonable time. A conductivity requirement may be used to ensure surface materials do not charge to high voltages, or store charge for long periods of time.
Document ID
19950010447
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Purvis, Carolyn K.
(NASA Lewis Research Center Cleveland, OH, United States)
Snyder, David B.
(NASA Lewis Research Center Cleveland, OH, United States)
Jongeward, Gary A.
(Maxwell Labs., Inc. La Jolla, CA., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
E-9258
NASA-TM-106794
NAS 1.15:106794
Report Number: E-9258
Report Number: NASA-TM-106794
Report Number: NAS 1.15:106794
Accession Number
95N16862
Funding Number(s)
PROJECT: RTOP 233-01-0E
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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