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Effects of high energy simulated space radiation on polymeric second-surface mirrorsA radiation effects experimental program was performed, in which second surface mirror type thermal control coatings were exposed to ultraviolet radiation, electrons, and protons simultaneously. Stability was assessed by making periodic spectral reflectance measurements in situ (and in air after testing for comparison). Solar absorption coefficients were derived by computer. Many of the exposed materials showed large amounts of degradation in reflectance absorptance, principally due to the electron exposure. A series of tests was conducted, leading to the identification of a modified second surface mirror that shows considerable improvement and promise for stability during thermal control applications in a charged particle space radiation environment.
Document ID
19760003890
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eogdall, L. B.
(Boeing Aerospace Co. Seattle, WA, United States)
Cannaday, S. S.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Space Radiation
Report/Patent Number
D180-18014-2
NASA-CR-132725
Report Number: D180-18014-2
Report Number: NASA-CR-132725
Accession Number
76N10978
Funding Number(s)
CONTRACT_GRANT: NAS1-13530
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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