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SiC Fiber-Reinforced Celsian CompositesCelsian is a promising matrix material for fiber-reinforced composites for high temperature structural applications. Processing and fabrication of small diameter multifilament silicon carbide tow reinforced celsian matrix composites are described. Mechanical and microstructural properties of these composites at ambient and elevated temperatures are presented. Effects of high-temperature exposures in air on the mechanical behavior of these composites are also given. The composites show mechanical integrity up to ~1100 C but degrade at higher temperatures in oxidizing atmospheres. A model has been proposed for the degradation of these composites in oxidizing atmospheres at high temperatures.
Document ID
20030093728
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Bansal, Narottam P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2003-212555
E-14121
NAS 1.15:212555
Report Number: NASA/TM-2003-212555
Report Number: E-14121
Report Number: NAS 1.15:212555
Funding Number(s)
WBS: WBS 22-708-31-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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