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Electrostatic discharge properties of selected Voyager spacecraft materialsTwelve material and component samples were exposed to an electron beam in order to measure the time history and amplitude of resultant electrostatic discharges. The typical experimental design was to mount the test article with its dielectric surface facing the beam and its conductive portion isolated from ground except by way of a shielded cable on which a discharged pulse could be observed. The behavior of the sample was then observed at bombarding energies from 20 to 100 keV in increasing 20 keV increments and then 90 to 30 keV in decreasing 20 keV increments. Observations were made at each energy for nominally two hours at an electron flux of 4 x 10 to the 9th power/sq cm/sec.
Document ID
19790015868
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barengoltz, J. B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Greegor, R. B., II
(Boeing Aerospace Co.)
Fogdall, L. B.
(Boeing Aerospace Co.)
Cannaday, S. S.
(Boeing Aerospace Co.)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Lewis Res. Center Spacecraft Charging Technol., 1978
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
79N24039
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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