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Environmental interactions and the SP-100 power systemInteractions of the SP-100 power system with its expected ambient environments are defined. SP-100 payloads will float 100 V negative of the low Earth orbit (LEO) plasma. Choice of proper geometries and materials will prevent arcing at conductor-insulator junctions in LEO. Care in selecting surface coatings will prevent dielectric breakdown. Sputtering is a concern for long-duration LEO missions. Atomic oxygen durability of SP-100 materials will be tested in ground and flight tests. Evaluation of SP-100 in lunar and planetary environments has begun. The report of a recent workshop on Chemical and Electrical Interactions on Mars identified many of the primary interactions.
Document ID
19930009688
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ferguson, Dale C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:105866
NASA-TM-105866
E-7328
Report Number: NAS 1.15:105866
Report Number: NASA-TM-105866
Report Number: E-7328
Accession Number
93N18877
Funding Number(s)
PROJECT: RTOP 590-13-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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