Study made of various propulsion and performance aspects of single-stage long range Mach 7 delta wing transport of 30,000 lb payload (125 passengers and cargo), encompasses consideration of propulsive performance of hypersonic ramjet design featuring lift augmentation; results indicate that 700,000-lb configuration could transport payload 3600 nautical mi with fuel reserve for descent and landing techniques similar to those presently used. (See also SAE -- Paper 427C for meeting Oct 9-13 1961 35 p)


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    Titel :

    Feasibility of Mach 7 transport employing airbreathing propulsion systems


    Weitere Titelangaben:

    SAE -- J


    Beteiligte:
    Pietrangeli, G.J. (Autor:in) / Nice, E.V. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Feasibility of Mach 7 transport employing airbreathing propulsion systems

    Pietrangeli, G.J. / Nice, E.V. | Engineering Index Backfile | 1961


    The Feasibility of a Mach 7 Transport Employing Airbreathing Propulsion Systems

    Nice, E. V. / Pietrangeli, G. J. | SAE Technical Papers | 1961



    Thermal management systems for high Mach airbreathing propulsion

    BERGHOLZ, ROBERT / HITCH, BRADLEY | AIAA | 1992


    Airbreathing Propulsion

    Springer Verlag | 2007