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Thermal blanket metallic film groundstrap and second surface mirror vulnerability to arc dischargesAvailable data on the geosynchronous orbit energetic plasma environment were examined, and a crude model was generated to permit an estimation to be made of the number of arc discharges per year to which a thermal blanket groundstrap would be subjected. Laboratory experiments and a survey of the literature on arc discharge characteristics were performed to define typical and worst case arc discharge current waveforms. In-air tests of different groundstrap configurations to a standardized test pulse were performed and a wide variability of durability values were found. A groundstrap technique, not used thus far, was found to be far superior than the others.
Document ID
19790015871
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Inouye, G. T.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Sanders, N. L.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Komatsu, G. K.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Valles, J. R.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Sellen, J. M., Jr.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
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
79N24042
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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