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Dielectric discharge characteristics in a two-electron simulation environmentThe results of a series of experiments in which flux levels representative of the space electron environment were used are presented and compared to the results of high flux tests. The simulation approach was to partition the space electron spectrum into two parts, those electrons which do not penetrate a material and therefore contribute to charging and those which completely penetrate the material. The nonpenetrating electrons were simulated using 25 keV electrons and the penetrating electrons by 350 keV electrons. The materials included in this investigation were Kapton, optical solar reflectors (OSRs), and a ground test satellite surface potential monitor which contained Kapton, astroquart, OSRs and teflon.
Document ID
19820006341
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Treadaway, M.
(JAYCOR Alexandria, VA, United States)
Leadon, R.
(JAYCOR Alexandria, VA, United States)
Mallon, C.
(JAYCOR Alexandria, VA, United States)
Flanagan, T.
(JAYCOR Alexandria, VA, United States)
Denson, R.
(JAYCOR Alexandria, VA, United States)
Wenaas, F.
(JAYCOR Alexandria, VA, 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
82N14214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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