The hydrogen oxygen engine used in the orbiter transfer vehicle is described. The engine design is analyzed and minimum engine performance and man rating requirements are discussed. Reliability and safety analysis test results are presented and payload, risk and cost, and engine installation parameters are defined. Engine tests were performed including performance analysis, structural analysis, thermal analysis, turbomachinery analysis, controls analysis, and cycle analysis.


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    Title :

    Orbit Transfer Vehicle (OTV) engine, phase A study. Volume 2: Study


    Contributors:

    Publication date :

    1979-06-29


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English