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Insulator edge voltage gradient effects in spacecraft charging phenomenaInsulating surfaces on geosynchronous satellites have been charged by geomagnetic substorms to a point where discharges occur. The electromagnetic pulses from these discharges couple into satellite electronic systems disrupting operations. 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 has been conducted to measure edge voltage gradients on silvered Teflon samples as they are charged by monoenergetic electron beams. It has been found that the surface voltage at insulator edges can be approximated by an exponential expression based on an electron current density balance. Using this expression at known breakdown conditions results in a discharge voltage gradient down the insulator edge to ground of about 150,000 V/cm.
Document ID
19790046126
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
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, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
December 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
79A30139
Distribution Limits
Public
Copyright
Other

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