A simplified model is presented of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at 25 different operating points of SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.


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    Title :

    Simplified Dynamic Model of the Space Shuttle Main Engine


    Contributors:
    A. Duyar (author) / V. Eldem (author) / W. Merrill (author) / T. Guo (author)

    Publication date :

    1991


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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