A mathematical model of the Space Shuttle Main Engine (SSME) as a complete assembly, with detailed emphasis on LOX and High Fuel Turbopumps is developed. The advantages of both complete engine dynamics, and high fidelity modeling are incorporated. Development of this model, some results, and projected applications are discussed.


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    Title :

    SSME structural dynamic model development


    Contributors:
    Foley, M. J. (author) / Tilley, D. M. (author) / Welch, C. T. (author)

    Publication date :

    1983-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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