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Microscopic evaluation of a polyimide (PMR-15)-graphite compositeAn effort to evaluate the high temperature performance of a polyimide (PMR-15)-graphite composite which consists of several plies of woven strands of carbon fibers was undertaken. The longterm effect of high temperature on the dry material was studied by exposing polished test specimens of 473 F in a oven for nearly 400 hours. Periodically the specimens were removed and observed microscopically. Gradually surface cracks began to appear and the number of cracks increased over time. At the conclusion of the exposure the specimens were graudually ground down and observed in order to determine the depth of the cracks into the interior of the material. This procedure was repeated at an exposure temperature of 550 F.
Document ID
19860001815
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fedderly, J. J.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Augl, J. M.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1985
Publication Information
Publication: NASA. Lewis Research Center High Temp. Polymer Matrix Composites
Subject Category
Composite Materials
Accession Number
86N11282
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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