The TF34 high bypass turbofan engine is being designed and developed to fulfill the powerplant requirements of the Navy's S-3A (VSX) aircraft. The Navy established specific requirements from the start of the development program to assure that the TF34 meets the very stringent demands of its carrier-based anti-submarine warfare environment. This paper discusses the selection of the optimum engine cycle and the aircraft mission analyses conducted to demonstrate that the selected engine met ASW mission requirements.


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    Titel :

    Design Considerations of the TF34-GE-2 High Bypass Turbofan Engine


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Niederer, P. (Autor:in) / Houlihan, R.E. (Autor:in)

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1969



    Erscheinungsdatum :

    1969-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch