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C/sic Life Prediction for Propulsion ApplicationsAccurate life prediction is critical to successful use of ceramic matrix composites (CMCs). The tools to accomplish this are immature and not oriented toward the behavior of carbon fiber reinforced silicon carbide (C/SiC), the primary system of interest for many reusable and single mission launch vehicle propulsion and airframe applications. This paper describes an approach and progress made to satisfy the need to develop an integrated life prediction system that addresses mechanical durability and environmental degradation of C/SiC.
Document ID
20040111984
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)
Verrilli, Michael J.
(NASA Glenn Research Center Cleveland, OH, United States)
Opila, Elizabeth J.
(NASA Glenn Research Center Cleveland, OH, United States)
Halbig, Michael C.
(Army Research Lab. Cleveland, OH, United States)
Calomino, Anthony M.
(NASA Glenn Research Center Cleveland, OH, United States)
Thomas, David J.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 29, 2003
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 713-82-32
Distribution Limits
Public
Copyright
Public Use Permitted.
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