This paper defines and evaluates auxiliary power systems for a self-sufficient 1975 fighter aircraft. The mission and auxiliary power requirements for a V/STOL fighter aircraft are used as a basis for this study. Candidate systems are identified and analyzed for their take-off gross weight penalty to the aircraft for missions requiring both short-time and long-time aircraft standby periods.The components of the various systems are evaluated as to their projected efficiency, weight, and size for use in the analysis. A recommended reference system is selected as the basis for an optimized system design. Specific areas of research and development are identified as required to obtain the advanced system components.


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    Titel :

    Auxiliary Power Systems for 1975 Fighter Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Meshew, A. D. (Autor:in) / Nicholls, B. H. (Autor:in)

    Kongress:

    National Air Transportation Meeting ; 1968



    Erscheinungsdatum :

    01.02.1968




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Auxiliary power systems for 1975 fighter aircraft

    Nicholis, B.N. / Meshew, A.D. | Engineering Index Backfile | 1968





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