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NASA NTRS ยท 19920051850

Ceramics and ceramic matrix composites - Aerospace potential and status

Abstract

Thermostructural ceramics and ceramic-matrix composites are attractive in numerous aerospace applications; the noncatastrophic fracture behavior and flaw-insensitivity of continuous fiber-reinforced CMCs renders them especially desirable. The present development status evaluation notes that, for most highly-loaded high-temperature applications, the requisite fiber-technology base is at present insufficient. In addition to materials processing techniques, the life prediction and NDE methods are immature and require a projection of 15-20 years for the maturity of CMC turbine rotors. More lightly loaded, moderate temperature aircraft engine applications are approaching maturity.

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BibTeXRIS

Levine, Stanley R.. 1992-01-01. Ceramics and ceramic matrix composites - Aerospace potential and status. https://ntrs.nasa.gov/citations/19920051850

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