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Overview of NASA's advanced high temperature engine materials technology programNASA's 'HITEMP' program has been charged with development of propulsion systems technologies for next-generation civil and military aircraft, stressing high-temperature/low-density composites. These encompass polymer-matrix composites for fans, ducts, and compressor cases, and intermetallic and metallic alloy matrix composites for applications in turbine disks, blades, and vanes, and ceramic matrix composites for combustors and turbines. An overview is presented of program concerns and achievements to date.
Document ID
19930069456
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ginty, Carol A.
(NASA Lewis Research Center Cleveland, OH, United States)
Gray, Hugh R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: International SAMPE Technical Conference, 24th and International SAMPE Metals and Metals Processing Conference, 3rd, Toronto, Canada, Oct. 20-22, 1992, Proceedings. Vol. 24 (A93-53376 23-23)
Publisher: Society for the Advancement of Material and Process Engineering
Subject Category
Chemistry And Materials (General)
Accession Number
93A53453
Distribution Limits
Public
Copyright
Other

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