NASA NTRS · 19930012923
Ceramic matrix composites (continuous fiber reinforced) thermal protection systems
Abstract
Concluded 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.
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Riccitiello, Salvatore R.. 1993-02-01. Ceramic matrix composites (continuous fiber reinforced) thermal protection systems. https://ntrs.nasa.gov/citations/19930012923
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