A conceptual design of a CTOL SETOLS CAS aircraft has been developed. The significant design feature is the use of a Surface Effect Takeoff and Landing System (SETOLS) in lieu of a normal landing gear. The SETOLS is an integral part of the point design, thereby achieving full design compatibility. This feature provides takeoff and landing capability, on the inflated rubber fabric type trunk installed on the bottom of the fuselage, from any unobstructed area such as water, grass, soil, etc. Effective operation is thereby achieved with a Conventional Takeoff and Landing (CTOL) aircraft design in the Close Air Support (CAS) mission from forward bases where time prevents construction and repair of long, hard surface runways. Advanced state-of-the-art design, appropriate for 1995 IOC, has been incorporated. One advanced technology Pratt & Whitney STF 529 turbofan is used for propulsion and trunk pressurization. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Conceptual Point Design Study of a New CTOL SETOLS CAS Aircraft for 1995 IOC


    Beteiligte:
    P. D. Sorensen (Autor:in) / R. L. Bayless (Autor:in) / E. F. Noel (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    219 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    V/STOL Capability by Modifying CTOL Aircraft

    Kuhn, R. E. | SAE Technical Papers | 1980


    CTOL transport aircraft characteristics, trends, and growth projections

    Aerospace Industries Association of America, Transport Aircraft Council | SLUB | 1973



    Short-haul CTOL aircraft research

    Williams, L. J. | NTRS | 1978