The high-pressure oxidizer turbopump (HPOTP) failure information propagation model (FIPM) is presented. The text includes a brief discussion of the FIPM methodology and the various elements which comprise a model. Specific details of the HPOTP FIPM are described. Listings of all the HPOTP data records are included as appendices.


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    Title :

    Studies and Analyses of the Space Shuttle Main Engine: High-Pressure Oxidizer Turbopump Failure Information Propagation Model


    Contributors:
    R. C. Glover (author) / S. W. Rudy (author) / A. E. Tischer (author)

    Publication date :

    1987


    Size :

    511 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English