Performance potential of liquid hydrogen fueled commercial transport operating in 1985-2000 time period is examined; mission analyses and design studies indicate 200 passenger, Mach 6 cruise, 5000 nautical mi range is reasonable compromise between economics, technology, and passenger appeal; crucial factor is cost of liquid hydrogen fuel. (31977)


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    Titel :

    Hydrogen fueled hypersonic treatment


    Weitere Titelangaben:

    ASME -- Aviation and Space -- Progress and Prospects


    Beteiligte:
    Jarlett, F.E. (Autor:in)

    Kongress:

    ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA



    Erscheinungsdatum :

    1968


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The hydrogen fueled hypersonic transport.

    Jarlett, F. E. | NTRS | 1968


    Structural concepts for hydrogen-fueled hypersonic airplanes

    Jackson, L. Robert / Davies, John G. / Wichorek, Gregory R. | TIBKAT | 1966


    Structural concepts for hydrogen-fueled hypersonic airplanes

    Davis, J. G., Jr. / Jackson, L. R. / Wichorek, G. R. | NTRS | 1966


    Structural Concepts for Hydrogen-Fueled Hypersonic Airplanes

    J. G. Davis / L. R. Jackson / G. R. Wichorek | NTIS | 1966


    Hydrogen Fueled Precooled Airbreathing Engines for Hypersonic Aircraft and Spaceplanes

    Hendrick, P. / Verstraete, D. | British Library Conference Proceedings | 2011