A hypersonic aircraft is designed which uses scramjets to accelerate from Mach 6 to Mach 10 and sustain that speed for two minutes. Different propulsion systems were considered and it was decided that the aircraft would use one full scale turbofan-ramjet. Two solid rocket boosters were added to save fuel and help the aircraft pass through the transonic region. After considering aerodynamics, aircraft design, stability and control, cooling systems, mission profile, and landing systems, a conventional aircraft configuration was chosen over that of a waverider. The conventional design was chosen due to its landing characteristics and the relative expense compared to the waverider. Fuel requirements and the integration of the engine systems and their inlets are also taken into consideration in the final design. A hypersonic aircraft was designed which uses scramjets to accelerate from Mach 6 to Mach 10 and sustain that speed for two minutes. Different propulsion systems were considered and a full scale turbofan-ramjet was chosen. Two solid rocket boosters were added to save fuel and help the aircraft pass through the transonic reqion. After the aerodynamics, aircraft design, stability and control, cooling systems, mission profile, landing systems, and their physical interactions were considered, a conventional aircraft configuration was chosen over that of a waverider. The conventional design was chosen due to its landing characteristics and the relative expense compared to the waverider. Fuel requirements and the integration of the engine systems and their inlets were also considered in the designing process.


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    Titel :

    Hypersonic aircraft design


    Beteiligte:
    Alkamhawi, Hani (Autor:in) / Greiner, Tom (Autor:in) / Fuerst, Gerry (Autor:in) / Luich, Shawn (Autor:in) / Stonebraker, Bob (Autor:in) / Wray, Todd (Autor:in)

    Erscheinungsdatum :

    1990-05-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hypersonic Aircraft Design

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

    Swithenbank, J. | Engineering Index Backfile | 1964


    Design of hypersonic aircraft

    Multhopp, H. | Engineering Index Backfile | 1961