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Feasibility of Kevlar 49/PMR-15 polyimide for high temperature applicationsKevlar 49 aramid organic fiber reinforced PMR-15 polyimide laminates were characterized to determine the applicability of the material to high temperature aerospace structures. Kevlar 49/3501-6 epoxy laminates were fabricated and characterized for comparison with the Kevlar 49/PMR-15 polyimide material. Flexural strengths and moduli and interlaminar shear strengths were determined from 75 to 600 F for the PMR-15 and from 75 to 450 F for the Kevlar 49/3501-6 epoxy material. The study also included the effects of hydrothermal and long-term elevated temperature exposures on the flexural strengths and moduli and the interlaminar shear strengths.
Document ID
19810059198
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hanson, M. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Subject Category
Composite Materials
Meeting Information
Meeting: National Technical Conference on Materials 1980
Location: Seattle, WA
Start Date: October 7, 1980
End Date: October 9, 1980
Accession Number
81A43602
Distribution Limits
Public
Copyright
Other

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