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Charging rates of metal-dielectric structuresMetal plates partially covered by 0.01-centimeter-thick fluorinated ethylene-propylene (FEP) Teflon were charged in the Lewis Research Center's geomagnetic substorm simulation facility using 5-, 8-, 10-, and 12-kilovolt electron beams. Surface voltage as a function of time was measured for various initial conditions (Teflon discharged or precharged) with the metal plate grounded or floating. Results indicate that both the charging rates and the levels to which the samples become charged are influenced by the geometry and initial charge state of the insulating surfaces. The experiments are described and the results are presented and discussed. NASA charging analyzer program (NASCAP) models of the experiments have been generated, and the predictions obtained are described. Implications of the study results for spacecraft are discussed.
Document ID
19790015862
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Purvis, C. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Staskus, J. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Roche, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Berkopec, F. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Spacecraft Charging Technol., 1978
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
79N24033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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