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Analysis of a space-exposed thermoplastic resinThe chemical characterization of a thermoplastic resin exposed to the low Earth orbit (LEO) environment for 10 months and for 5.8 years is reported. The resin, processed as a thick film and as a matrix for a graphite fiber reinforced composite, few exposed in the RAM direction on the NASA Long Duration Exposure Facility (LDEF). Differences attributable to environmental exposure were detected in infrared spectra and in various molecular weight parameters of film after 10 months in LEO. Those effects were not as apparent in composites after 5.8 years in LEO. Increased exposure to atomic oxygen toward the end of the LDEF mission probably scrubbed these effects from specimens exposed for 5.8 years. The intent of this study is to increase our fundamental understanding of space environmental effects on polymeric materials and to develop a benchmark for enhancing our methodology for and understanding of the ground-based simulation of space environmental effects.
Document ID
19930069393
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Young, Philip R.
(NASA Langley Research Center Hampton, VA, United States)
Slemp, Wayne S.
(NASA Langley Research Center Hampton, VA, United States)
Siochi, Emilie J.
(NASA Langley Research Center Hampton, VA, United States)
Davis, Judith R. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: International SAMPE Technical Conference, 24th and International SAMPE Metals and Metals Processing Conference, 3rd, Toronto, Canada, Oct. 20-22, 1992, Proceedings. Vol. 24 (A93-53376 23-23)
Publisher: Society for the Advancement of Material and Process Engineering
Subject Category
Nonmetallic Materials
Accession Number
93A53390
Distribution Limits
Public
Copyright
Other

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