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Review of thermal properties of graphite composite materialsFlammability, thermal, and selected mechanical properties of composites fabricated with epoxy and other thermally stable resin matrices are described. Properties which were measured included limiting-oxygen index, smoke evolution, thermal degradation products, total-heat release, heat-release rates, mass loss, flame spread, ignition resistance, thermogravimetric analysis, and selected mechanical properties. The properties of 8 different graphite composite panels fabricated using four different resin matrices and two types of graphite reinforcement are described. The resin matrices included: XU71775/H795, a blend of vinyl polystyryl pyridine and bismaleimide; H795, a bismaleimide; Cycom 6162, a phenolic; and PSP 6022M, a polystyryl pyridine. The graphite fiber used was AS-4 in the form of either tape or fabric. The properties of these composites were compared with epoxy composites. It was determined that the blend of vinyl polystyryl pyridine and bismaleimide (XU71775/H795) with the graphite tape was the optimum design giving the lowest heat release rate.
Document ID
19880007441
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kourtides, D. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1987
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:100049
NASA-TM-100049
Accession Number
88N16825
Funding Number(s)
PROJECT: RTOP 506-43-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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