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Ultra-high Temperature Ceramic Composites for Leading Edges, 2004Ultrahigh temperature ceramics (UHTC) have performed unreliably due to material flaws and attachment design. These deficiencies are brought to the fore by the low fracture toughness and thermal shock resistance of the UHTC. If these deficiencies are overcome, we are still faced with poor oxidation resistance as a limitation on UHTC applicability to reusable launch vehicles. We have been addressing the deficiencies of UHTC for the past two years via a small task at GRC that is in the Airframe part of the Next Generation Launch Technology Program. Our focus is on composite constructions and functional grading to address the mechanical issues and on composition modification to address the oxidation issue. The progress on approaches to improving oxidation resistance by alloying and functional grading will be reported.
Document ID
20040111983
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Levine, Stanley R.
(NASA Glenn Research Center Cleveland, OH, United States)
Opila, Elizabeth J.
(NASA Glenn Research Center Cleveland, OH, United States)
Lorincz, Jonathan A.
(QSS Group, Inc. Cleveland, OH, United States)
Singh, Mrityunjay
(QSS Group, Inc. Cleveland, OH, United States)
Robinson, Raymond C.
(QSS Group, Inc. Cleveland, OH, United States)
Ellerby, Donald T.
(NASA Ames Research Center Moffett Field, CA, United States)
Gasch, Matthew J.
(Eloret Corp. Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Meeting Information
Meeting: 28th Annual Conference on Composites, Materials and Structures
Location: Cape Canaveral, FL
Country: United States
Start Date: January 25, 2004
End Date: January 30, 2004
Sponsors: Ceramic, Metal and Carbon Composites Committee
Funding Number(s)
WBS: WBS 22-713-76-32
Distribution Limits
Public
Copyright
Public Use Permitted.
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