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High temperature metal matrix composites for future aerospace systemsResearch was conducted on metal matrix composites and intermetallic matrix composites to understand their behavior under anticipated future operating conditions envisioned for aerospace power and propulsion systems of the 21st century. Extremes in environmental conditions, high temperature, long operating lives, and cyclic conditions dictate that the test evaluations not only include laboratory testing, but simulated flight conditions. The various processing techniques employed to fabricate composites are discussed along with the basic research underway to understand the behavior of high temperature composites, and the relationship of this research to future aerospace systems.
Document ID
19880001556
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stephens, Joseph R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-100212
NAS 1.15:100212
E-3821
Report Number: NASA-TM-100212
Report Number: NAS 1.15:100212
Report Number: E-3821
Accession Number
88N10938
Funding Number(s)
PROJECT: RTOP 505-63-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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