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Hybridized polymer matrix compositesDesign approaches and materials are described from which are fabricated pyrostatic graphite/epoxy (Gr/Ep) laminates that show improved retention of graphite particulates when subjected to burning. Sixteen hybridized plus two standard Gr/Ep laminates were designed, fabricated, and tested in an effort to eliminate the release of carbon (graphite) fiber particles from burned/burning, mechanically disturbed samples. The term pyrostatic is defined as meaning mechanically intact in the presence of fire. Graphite particulate retentive laminates were constructed whose constituent materials, cost of fabrication, and physical and mechanical properties were not significantly different from existing Gr/Ep composites. All but one laminate (a Celion graphite/bis-maleimide polyimide) were based on an off-the-shelf Gr/Ep, the AS-1/3501-5A system. Of the 16 candidates studied, four thin (10-ply) and four thick (50-ply) hybridized composites are recommended.
Document ID
19810022818
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
London, A.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA-CR-165339
Report Number: NASA-CR-165339
Accession Number
81N31361
Funding Number(s)
CONTRACT_GRANT: NAS3-21382
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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