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Ethynylated aromatics as high temperature matrix resinsDifunctional and trifunctional arylacetylenes were used as monomers to form thermoset matrix resin composites. Composites can be hot pressed at 180 C to react 80 percent of the acetylene groups. Crosslinking is completed by postcuring at 350 C. The postcured resins are thermally stable to nominally 460 C in air. As a result of their high crosslink density, the matrix exhibits brittle failure when unaxial composites are tested in tension. Failure of both uniaxial tensile and flexural specimens occurs in shear at the fiber matrix interface. Tensile fracture stresses for 0 deg composites fabricated with 60 v/o Celion 6K graphite fiber were 827 MPa. The strain to failure was 0.5 percent. Composites fabricated with 8 harness satin Celion cloth (Fiberite 1133) and tested in tension also failed in shear at tensile stresses of 413 MPa.
Document ID
19880009256
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hurwitz, Frances I.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1986
Subject Category
Composite Materials
Report/Patent Number
E-3480
NASA-TM-89829
NAS 1.15:89829
Report Number: E-3480
Report Number: NASA-TM-89829
Report Number: NAS 1.15:89829
Accession Number
88N18640
Funding Number(s)
PROJECT: RTOP 506-43-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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