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Composite materials flown on the Long Duration Exposure FacilityOrganic composite test specimens were flown on several LDEF experiments. Both bare and coated composites were flown. Atomic oxygen eroded bare composite material, with the resins being recessed at a greater rate than the fibers. Selected coating techniques protected the composite substrate in each case. Tensile and optical properties are reported for numerous specimens. Fiberglass and metal matrix composites were also flown.
Document ID
19950018163
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
George, Pete E.
(Boeing Defense and Space Group Seattle, WA, United States)
Dursch, Harry W.
(Boeing Defense and Space Group Seattle, WA, United States)
Pippin, H. Gary
(Boeing Defense and Space Group Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1995
Publication Information
Publisher: NASA
Subject Category
Chemistry And Materials (General)
Report/Patent Number
NAS 1.26:4657
NASA-CR-4657
Report Number: NAS 1.26:4657
Report Number: NASA-CR-4657
Accession Number
95N24583
Funding Number(s)
CONTRACT_GRANT: NAS1-18224
CONTRACT_GRANT: NAS1-19247
PROJECT: RTOP 506-43-61-02
PROJECT: RTOP 233-03-02-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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