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Evaluation of 2D ceramic matrix composites in aeroconvective environmentsAn evaluation is conducted of a novel ceramic-matrix composite (CMC) material system for use in the aeroconvective-heating environments encountered by the nose caps and wing leading edges of such aerospace vehicles as the Space Shuttle, during orbit-insertion and reentry from LEO. These CMCs are composed of an SiC matrix that is reinforced with Nicalon, Nextel, or carbon refractory fibers in a 2D architecture. The test program conducted for the 2D CMCs gave attention to their subsurface oxidation.
Document ID
19930069462
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Riccitiello, Salvatore R. (NASA Ames Research Center Moffett Field, CA, United States)
Love, Wendell L. (NASA Ames Research Center Moffett Field, CA, United States)
Balter-Peterson, Aliza (Eloret Inst. Sunnivale, CA, 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
Composite Materials
Accession Number
93A53459
Funding Number(s)
CONTRACT_GRANT: NAS2-12996
Distribution Limits
Public
Copyright
Other

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