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Material Selection Guidelines to Limit Atomic Oxygen Effects on Spacecraft SurfacesThis report provides guidelines in selecting materials for satellites and space platforms, designed to operate within the Low-Earth orbit environment, which limit the effects of atomic oxygen interactions with spacecraft surfaces. This document should be treated as an introduction rather than a comprehensive guide since analytical and flight technologies continue to evolve, flight experiments are conducted as primary or piggyback opportunities arise, and our understanding of materials interactions and protection methods grows. The reader is urged to consult recent literature and current web sites containing information about research and flight results.
Document ID
19990064119
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Dooling, D.
(D2 Associates Huntsville, AL United States)
Finckenor, M. M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1999
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TP-1999-209260
NAS 1.60:209260
M-922
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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