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Characterization of Damage Accumulation in a C/SiC Composite at Elevated TemperaturesThis research is part of a program aimed to evaluate and demonstrate the ability of candidate CMC materials for a variety of applications in reusable launch vehicles. The life and durability of these materials in rocket and engine applications are of major concern and there is a need to develop and validate life prediction methodology. In this study, material characterization and mechanical testing was performed in order to identify the failure modes, degradation mechanisms, and progression of damage in a C/SiC composite at elevated temperatures. The motivation for this work is to provide the relevant damage information that will form the basis for the development of a physically based life prediction methodology.
Document ID
19970024966
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Telesman, Jack
(NASA Lewis Research Center Cleveland, OH United States)
Verrilli, Mike
(NASA Lewis Research Center Cleveland, OH United States)
Ghosn, Louis
(Case Western Reserve Univ. Cleveland, OH United States)
Kantzos, Pete
(Ohio Aerospace Inst. Cleveland, OH United States)
Date Acquired
August 17, 2013
Publication Date
April 1, 1997
Publication Information
Publication: Physics and Process Modeling (PPM) and Other Propulsion R and T
Volume: 1
Subject Category
Composite Materials
Report/Patent Number
Paper-11-Vol-1
Accession Number
97N24665
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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