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Calculation of surface current response to surface flashover of a large sample under grounded and floating conditionsResults for the electromagnetic response to the discharge of an 80 cm diameter dielectric sample mounted on a 120 cm diameter cylinder are presented. It is assumed that the dielectric is charged with a known potential profile dropping sharply near the edge, and the substrate initially grounded. During the early part of the discharge (approximately 10 ns) there is little difference between the grounded and floating cases. Beyond about 10 ns the grounded experiment is in approximate steady state, continuous to blow off charge until the dielectric is substantially discharged. The floating case, however, shows modestly decreasing emission and response. Eventually, a quasi-steady state is reached in which charge is transported from dielectric to substrate rather than blown off.
Document ID
19820006386
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mandell, M. J.
(Systems Science and Software San Diego, CA, United States)
Katz, I.
(Systems Science and Software San Diego, CA, United States)
Schnuelle, G. W.
(Systems Science and Software San Diego, CA, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1980
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Charging Technol., 1980
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
82N14259
Funding Number(s)
CONTRACT_GRANT: DNA001-79-C-0027
CONTRACT_GRANT: DNA001-79-C-0079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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