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NASCAP charging calculations for a synchronous orbit satelliteThe use of the NASA Charging Analyzer Program (NASCAP) for the computation of spacecraft charge up in the energetic plasma environment of geosynchronous orbits is described. Spacecraft modelling, materials parameters, and NASCAP charging analyses are described. The synchronous orbit plasma environment used in the stress analysis employs a two Maxwellian energy distribution to determine the fluxes. Several NASCAP runs performed to determine the location and magnitude of environmentally induced voltage stresses are analyzed.
Document ID
19820006383
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sanders, N. L.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Inouye, G. T.
(TRW Defense and Space Systems Group Redondo Beach, 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
82N14256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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