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    Fiber-Reinforced Superalloys For Rocket Engines (1990)
    In:  Other Sources
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    Publication Date: 2019-07-12
    Description: Report discusses experimental studies of fiber-reinforced superalloy (FRS) composite materials for use in turbine blades in rocket engines. Intended to withstand extreme conditions of high temperature, thermal shock, atmospheres containing hydrogen, high cycle fatigue loading, and thermal fatigue, which tax capabilities of even most-advanced current blade material - directionally-solidified, hafnium-modified MAR M-246 {MAR M-246 (Hf) (DS)}. FRS composites attractive combination of properties for use in turbopump blades of advanced rocket engines at temperatures from 870 to 1,100 degrees C.
    Keywords: MATERIALS
    Type: LEW-14871 , NASA Tech Briefs (ISSN 0145-319X); 14; 7; P. 58
    Format: text
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    NASA TECHNICAL REPORTS
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