Three lift/propulsion concepts for a V/STOL supersonic combat aircraft have been compared. The intention was to show the effect of the propulsion system on aircraft weight and size, performance, and life cycle costs for: For a postulated deck-launched intercept mission, the vectored thrust propulsion system with Plenum Chamber Burning gives the smallest and cheapest aircraft having the required performance. In addition, for a given take-off ground run the vectored thrust powered aircraft has the longest fighter escort mission radius.


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    Titel :

    A Comparison of Propulsion Systems for V/STOL Supersonic Combat Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Simpkin, P. (Autor:in) / Lewis, W. J. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1980



    Erscheinungsdatum :

    1980-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    STOL propulsion systems

    Denington, R. J. / Koenig, R. W. / Vanco, M. R. et al. | NTRS | 1972


    Lift fan propulsion systems-V/STOL aircraft control

    Beeler, E.F. / Volk, L.J. | Engineering Index Backfile | 1965


    LIFT FAN PROPULSION SYSTEMS V/STOL AIRCRAFT CONTROL

    BEELER, E. F. / VOLK, L. J. | SAE Technical Papers | 1965


    Analysis of propulsion systems for V/STOL aircraft

    Wadkovsky, A. | Engineering Index Backfile | 1964