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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    Titel :

    Studies and analyses of the space shuttle main engine: High-pressure oxidizer turbopump failure information propagation model


    Beteiligte:
    Glover, R. C. (Autor:in) / Rudy, S. W. (Autor:in) / Tischer, A. E. (Autor:in)

    Erscheinungsdatum :

    20.04.1987


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch