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Simulation of space radiation effects on polyimide film materials for high temperature applicationsSpace environment effects on candidate materials for the solar sail film are determined. Polymers, including metallized polyimides that might be suitable solar radiation receivers, were exposed to combined proton and solar electromagnetic radiation. Each test sample was weighted, to simulate the tension on the polymer when it is stretched into near-planar shape while receiving solar radiation. Exposure rates up to 16 times that expected in Earth orbit were employed, to simulate near-sun solar sailing conditions. Sample appearance, elongation, and shrinkage were monitored, noted, and documented in situ. Thermosetting polyimides showed less degradation or visual change in appearance than thermoplastics.
Document ID
19780020661
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fogdall, 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
November 1, 1977
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-CR-157322
Report Number: NASA-CR-157322
Accession Number
78N28604
Funding Number(s)
CONTRACT_GRANT: JPL-954701
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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