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.


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    Titel :

    Fiber-Reinforced Superalloys For Rocket Engines


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1990-07-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Fiber-reinforced, high-performance superalloys

    Zanchuk, W.A. | Tema Archiv | 1988


    Rocket Engines

    K. Bi-Tien | NTIS | 1976


    Rocket Engines

    by Feng Wen-Lan | NTIS | 1968


    Rocket engines

    Allen, S. | Engineering Index Backfile | 1957


    Rocket Engines

    T. M. Melkumov / N. I. Melik-Pashaev / P. G. Chistyakov et al. | NTIS | 1969