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High temperature, short term tensile strength of C6000/PMR-15 compositesTensile tests were conducted on 0 unidirectionally reinforced Celion 6000 graphite fibers in PMR-15 polyimide matrix. Tensile strengths for coupons subjected to short and long term uniform temperatures were obtained. Thick coupons, heated on one side to produce significant transient through thickness temperature gradients, were tested and compared to the strength of specimens with uniform temperature distributions. All coupons were radiantly heated and reached maximum test temperatures within 15 sec. Tensile loads were applied to the coupons after 15 sec of elevated temperature exposure. Loading rates were selected so that specimen failures occurred within a maximum of 45 sec after reaching the test temperature. Results indicate that significant tensile strength remains beyond the material post cure temperature.
Document ID
19860001812
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Digiovanni, P. R.
(Raytheon Co. Bedford, MA, United States)
Paterson, D.
(Raytheon Co. Bedford, MA, 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
86N11279
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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