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Ceramic matrix composites (continuous fiber reinforced) thermal protection systemsConcluded remarks are: (1) advanced carbon-carbon (ACC) substrate fabrication technology in good shape; (2) ACC coating improvements satisfactory but additional work needed; (3) non-destructive test techniques to monitor hardware during operational life needed; and (4) cost reduction approaches a high priority.
Document ID
19930012923
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Riccitiello, Salvatore R. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Space Transportation Materials and Structures Technology Workshop. Volume 2: Proceedings
Subject Category
Composite Materials
Accession Number
93N22112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930012892Collected WorksSpace Transportation Materials and Structures Technology Workshop
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