Promising applications for aircraft capable of hypersonic speeds, i.e., Mach 5 plus, can be divided into boost and cruise applications, although boost type aircraft could have long range capability by orbiting to its destination; typical flight corridors are shown for cruise and boost applications, plotted as flight altitude vs flight Mach number; integrated vehicle design considerations; possible air-breathing engines for hypersonic propulsion include precooled turbojet with reheat, turbo-rocket, liquid air cycle engines, and ramjet; problem of mixing fuel and air sufficiently quickly.


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    Titel :

    Design of hypersonic aircraft


    Weitere Titelangaben:

    Shell Aviation News


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Hypersonic Aircraft Design

    H. Alkamhawi / T. Greiner / G. Fuerst et al. | NTIS | 1990


    Hypersonic aircraft design

    Alkamhawi, Hani / Greiner, Tom / Fuerst, Gerry et al. | NTRS | 1990


    Advanced hypersonic aircraft design

    Utzinger, Rob / Blank, Hans-Joachim / Cox, Craig et al. | NTRS | 1992


    Advanced Hypersonic Aircraft Design

    R. Utzinger / H. Blank / C. Cox et al. | NTIS | 1992


    Design of hypersonic aircraft

    Multhopp, H. | Engineering Index Backfile | 1961