NASA NTRS · 19930035505
Ceramic matrix composite applications in advanced liquid fuel rocket engine turbomachinery
Abstract
Fiber-reinforced ceramic matrix composites have been identified with properties suitable for near term applications. Conceptual design studies indicate the feasibility of applying C/SiC, and subelements were manufactured that verify selected fabrication features and key material properties. Tests and inspection of these subelements confirmed their capabilities.
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Brockmeyer, Jerry W.. 1992-06-01. Ceramic matrix composite applications in advanced liquid fuel rocket engine turbomachinery. https://ntrs.nasa.gov/citations/19930035505
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