Data on the performance, stability, and thermal characteristics of an OME operating with an alternate injector configuration and with alternate propellants was obtained. The design, manufacturing, and operating characteristics of an electroformed, regeneratively cooled thrust chamber were also derived. Subscale and full scale tests provide data relating to off-design and transient operation. (Author)


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    Title :

    Space Shuttle Orbit Maneuvering Engine


    Contributors:

    Publication date :

    1975


    Size :

    214 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English