Normal modes of the blades and nozzles of the HPFTP and HPOTP are defined and potential driving forces for the blades are identified. The computer models used in blade analyses are described, with results. Similar information is given for the nozzles.


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    Title :

    Space Shuttle Main Engine Powerhead Structural Modeling, Stress and Fatigue Life Analysis. Volume 2: Dynamics of Blades and Nozzles SSME HPFTP and HPOTP


    Contributors:
    J. C. Hammett (author) / C. H. Hayes (author) / J. M. Price (author) / J. K. Robinson (author) / G. A. Teal (author)

    Publication date :

    1983


    Size :

    130 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English