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Space environmental effects on polymeric materialsPolymeric materials that may be exposed on spacecraft to the hostile environment beyond Earth's atmosphere were subjected to atomic oxygen, electron bombardment, and ultraviolet radiation in terrestrial experiments. Evidence is presented for the utility of an inexpensive asher for determining the relative susceptibility of organic polymers to atomic oxygen. Kapton, Ultem, P1700 polysulfone, and m-CBB/BIS-A (a specially formulated polymer prepared at NASA Langley) all eroded at high rates, just as was observed in shuttle experiments. Films of Ultem, P1700 polysulfone, and m-CBB/BIS-A were irradiated with 85 keV electrons. The UV/VIS absorbance of Ultem was found to decay with time after irradiation, indicating free radical decay. The tensile properties of Ultem began to change only after it had been exposed to 100 Mrads. The effects of dose rate, temperature, and simultaneous vs. sequential electron and UV irradiation were also studied.
Document ID
19880007495
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kiefer, Richard L.
(College of William and Mary Williamsburg, VA, United States)
Orwoll, Robert A.
(College of William and Mary Williamsburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.26:182454
NASA-CR-182454
Report Number: NAS 1.26:182454
Report Number: NASA-CR-182454
Accession Number
88N16879
Funding Number(s)
CONTRACT_GRANT: NAG1-678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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