Conceptual Study on hypersonic airplanes using pre-cooled turbojet

Hideyuki Taguchi, Akira Murakami, Tetsuya Satou, Takeshi Tsuchiya

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    8 Citations (Scopus)

    Abstract

    Conceptual Study on hypersonic airplanes with Mach 5 cruising capability is performed in order to improve the speed of intercontinental air transportations. Requirements for engine performance, thrust to mass ratio and heat resistant structure are discussed. As a result, reference concept of a hypersonic airplane with pre-cooled turbojet engine with liquid hydrogen fuel is shown. Then, a small hypersonic flight experiment is planned for demonstration of Mach 5 cruising technologies. Aerodynamic shape of the experimental vehicle is examined by CFD and wind tunnel tests.

    Original languageEnglish
    Title of host publication15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
    Publication statusPublished - 2008
    Event15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference - Dayton, OH
    Duration: 2008 Apr 282008 May 1

    Other

    Other15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
    CityDayton, OH
    Period08/4/2808/5/1

    Fingerprint

    Hypersonic aerodynamics
    Aircraft
    Mach number
    Turbojet engines
    Hydrogen fuels
    Liquid fuels
    Wind tunnels
    Aerodynamics
    Computational fluid dynamics
    Demonstrations
    Engines
    Experiments

    ASJC Scopus subject areas

    • Engineering(all)

    Cite this

    Taguchi, H., Murakami, A., Satou, T., & Tsuchiya, T. (2008). Conceptual Study on hypersonic airplanes using pre-cooled turbojet. In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference [2008-2503]

    Conceptual Study on hypersonic airplanes using pre-cooled turbojet. / Taguchi, Hideyuki; Murakami, Akira; Satou, Tetsuya; Tsuchiya, Takeshi.

    15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 2008. 2008-2503.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Taguchi, H, Murakami, A, Satou, T & Tsuchiya, T 2008, Conceptual Study on hypersonic airplanes using pre-cooled turbojet. in 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference., 2008-2503, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, 08/4/28.
    Taguchi H, Murakami A, Satou T, Tsuchiya T. Conceptual Study on hypersonic airplanes using pre-cooled turbojet. In 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 2008. 2008-2503
    Taguchi, Hideyuki ; Murakami, Akira ; Satou, Tetsuya ; Tsuchiya, Takeshi. / Conceptual Study on hypersonic airplanes using pre-cooled turbojet. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 2008.
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