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High temperature polymer matrix compositesWith the increased emphasis on high performance aircraft the need for lightweight, thermal/oxidatively stable materials is growing. Because of their ease of fabrication, high specific strength, and ability to be tailored chemically to produce a variety of mechanical and physical properties, polymers and polymer matrix composites present themselves as attractive materials for a number of aeropropulsion applications. In the early 1970s researchers at the NASA Lewis Research Center developed a highly processable, thermally stable (600 F) polyimide, PMR-15. Since that time, PMR-15 has become commercially available and has found use in military aircraft, in particular, the F-404 engine for the Navy's F/A-18 strike fighter. The NASA Lewis'contributions to high temperature polymer matrix composite research will be discussed as well as current and future directions.
Document ID
19880007317
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meador, Michael A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1987
Publication Information
Publication: Aeropropulsion '87. Session 1: Aeropropulsion Materials Research
Subject Category
Composite Materials
Accession Number
88N16700
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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