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Advanced ceramic matrix composites for TPSRecent advances in ceramic matrix composite (CMC) technology provide considerable opportunity for application to future aircraft thermal protection system (TPS), providing materials with higher temperature capability, lower weight, and higher strength and stiffness than traditional materials. The Thermal Protection Material Branch at NASA Ames Research Center has been making significant progress in the development, characterization, and entry simulation (arc-jet) testing of new CMC's. This protection gives a general overview of the Ames Thermal Protection Materials Branch research activities, followed by more detailed descriptions of recent advances in very-high temperature Zr and Hf based ceramics, high temperature, high strength SiC matrix composites, and some activities in polymer precursors and ceramic coating processing. The presentation closes with a brief comparison of maximum heat flux capabilities of advanced TPS materials.
Document ID
19930003262
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rasky, Daniel J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Publication Information
Publication: NASA. Langley Research Center, Current Technology for Thermal Protection Systems
Subject Category
Composite Materials
Accession Number
93N12450
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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