There is a current need for a low cost, low maintenance, unmanned High Altitude Long Endurance (HALE) aircraft to conduct high altitude atmospheric studies. Future military applications are possible. The preliminary design of a HALE vehicle is presented with special attention to low cost (low maintenance, low support requirements) and manufacturability. Emphasis is also placed on the propulsion system design, using an advanced ducted engine for low noise and improved propulsive efficiency.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of a High Altitude Long Endurance Aircraft with Manufacturing Considerations


    Beteiligte:
    C. Grant (Autor:in) / R. Hazlewood (Autor:in) / H. Sacks (Autor:in) / T. Downen (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    High Altitude Long Endurance Aircraft Design Studies

    Venkayya, V. B. / Tischler, V. A. / North Atlantic Treaty Organization | British Library Conference Proceedings | 1993



    High Altitude Long Endurance Aircraft

    Kaempf, P. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2000