The potential was examined of hydrogen-fueled supersonic vehicles designed for cruise at Mach 2.7 and at Mach 2.2. The aerodynamic, weight, and propulsion characteristics of a previously established design of a LH2 fueled, Mach 2.7 supersonic cruise vehicle (SCV) were critically reviewed and updated. The design of a Mach 2.2 SCV was established on a corresponding basis. These baseline designs were then studied to determine the potential of minimizing energy expenditure in performing their design mission, and to explore the effect of fuel price and noise restriction on their design and operating performance. The baseline designs of LH2 fueled aircraft were than compared with equivalent designs of jet A (conventional hydrocarbon) fueled SCV's. Use of liquid hydrogen for fuel for the subject aircraft provides significant advantages in performance, cost, noise, pollution, sonic boom, and energy utilization. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Minimum Energy, Liquid Hydrogen Supersonic Cruise Vehicle Study


    Beteiligte:
    G. D. Brewer (Autor:in) / R. E. Morris (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    178 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Minimum energy, liquid hydrogen supersonic cruise vehicle study

    Brewer, G. D. / Morris, R. E. | NTRS | 1975



    Supersonic cruise Technology

    MacLean, F. E. / USA, National Aeronautics and Space Administration | TIBKAT | 1985


    Supersonic cruise inlets

    Bowditch, D. N. / Coltrin, R. E. / Sanders, B. W. et al. | NTRS | 1971


    Supersonic Cruise Technology

    Mclean, F. Edward | NTRS | 1985