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Insulator edge voltage gradient effects in spacecraft charging phenomenaInsulating surfaces on geosynchronous satellites were charged by geomagnetic substorms to a point where discharges occur. The electromagnetic pulses from these discharges couple into satellite electronic systems disrupting operations are examined. Laboratory tests conducted on insulator charging have indicated that discharges appear to be initiated at insulator edges where voltage gradients can exist. An experimental investigation was conducted to measure edge voltage gradients on silvered Teflon samples as they are charged by monoenergetic electron beams. It was found that the surface voltage at insulator edges can be approximated by an exponential expression based on an electron current density balance.
Document ID
19790002938
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stevens, N. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Purvis, C. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Staskus, J. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
E-9769
NASA-TM-78988
Report Number: E-9769
Report Number: NASA-TM-78988
Meeting Information
Meeting: Ann. Conf. on Nucl. and Space Radiation Effects
Location: Albuquerque, NM
Country: United Stataes
Start Date: July 18, 1978
End Date: July 21, 1978
Sponsors: IEEE
Accession Number
79N11109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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