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NASCAP modelling computations on large optics spacecraft in geosynchronous substorm environmentsThe NASA Charging Analyzer Program (NASCAP) is used to evaluate qualitatively the possibility of such enhanced spacecraft contamination on a conceptual version of a large satellite. The evaluation is made by computing surface voltages on the satellite due to encounters with substorm environments and then computing charged particle trajectories in the electric fields around the satellite. Particular attention is paid to the possibility of contaminants reaching a mirror surface inside a dielectric tube because this mirror represents a shielded optical surface in the satellite model used. Deposition of low energy charged particles from other parts of the spacecraft onto the mirror was found to be possible in the assumed moderate substorm environment condition. In the assumed severe substorm environment condition, however, voltage build up on the inside and edges of the dielectric tube in which the mirror is located prevents contaminants from reaching the mirror surface.
Document ID
19800009830
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stevens, N. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Purvis, C. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81395
E-305
Report Number: NASA-TM-81395
Report Number: E-305
Meeting Information
Meeting: Soc. of Photo-Optical Instrumentation Engineers, Los Angeles Technical Symp.
Location: North Hollywood, CA
Country: United States
Start Date: February 4, 1980
End Date: February 7, 1980
Accession Number
80N18095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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