Rocketdyne, under contract to NASA-Lewis Research Center, is engaged in developing the technology for major subsystems of a small, high-performance, liquid rocket engine with the capabilities required for high-energy, upper-stage applications. Included in these efforts are the high-pressure turbopumps, preburner, igniter components, and high-area-ratio thrust chamber. A brief description of the engine system and its subsystems is given. The status of the programs is reviewed and the results of the testing conducted are presented.


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    Titel :

    Small, high-performance engine component technology status


    Beteiligte:
    Yost, M. C. (Autor:in) / Csomor, A. (Autor:in)

    Kongress:

    Propulsion Conference ; 1976 ; Palo Alto, CA


    Erscheinungsdatum :

    01.07.1976


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






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