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Polyimide composites: Application historiesAdvanced composite hardware exposed to thermal environments above 127 C (260 F) must be fabricated from materials having resin matrices whose thermal/moisture resistance is superior to that of conventional epoxy-matrix systems. A family of polyimide resins has evolved in the last 10 years that exhibits the thermal-oxidative stability required for high-temperature technology applications. The weight and structural benefits for organic-matrix composites can now be extended by designers and materials engineers to include structures exposed to 316 F (600 F). Polyimide composite materials are now commercially available that can replace metallic or epoxy composite structures in a wide range of aerospace applications.
Document ID
19860001819
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Poveromo, L. M.
(Grumman Aerospace Corp. Bethpage, NY, 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
86N11286
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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