Design and parametric data for the hydrogen oxygen engine used in the orbiter transfer vehicle are presented. The engine design is analyzed and minimum engine performance and man rating requirements are discussed. Candidate cycle performance, weight and tradeoff analysis, and cost estimates are reported.


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    Title :

    Orbit Transfer Vehicle (OTV) engine, phase A study. Volume 1: Executive Summary


    Contributors:

    Publication date :

    1979-06-29


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English