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.
Fiber-Reinforced Superalloys For Rocket Engines
NASA Tech Briefs ; 14 , 7
1990-07-01
Miscellaneous
No indication
English
Fiber-reinforced, high-performance superalloys
Tema Archive | 1988
|Engineering Index Backfile | 1957
|Engineering Index Backfile | 1957
|NTIS | 1968
|Engineering Index Backfile | 1957
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