Research and development of ramjet engine for high-mach integrated control experiment (HIMICO)

Sho Wakabayashi, Hidekazu Yoshida, Takahiro Chiga, Tetsuya Satou, Hideyuki Taguchi, Takayuki Kojima, Toshiki Okamoto, Yutaka Ikeda, Shinji Nakaya, Mitsuhiro Tsue

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

    Abstract

    The HIMICO (High-Mach Integrated Control experiment) project is under way by universities and JAXA. The purposes are to establish the flying test bed of hypersonic flight experiments and to demonstrate the integration control technology of the airframe and the engine. Currently, the performance of the ramjet engine for HIMICO is being acquired and improved. Two kinds of verification experiment are shown here: a supersonic wind tunnel test and a combustion test. On the supersonic wind tunnel test, the performance maps of the air-intake are acquired at Mach 3.0, 3.4 and 3.8. The condition of the buzz occurring is investigated. We should decide the flight experimental conditions of the engine under which the buzz does not occur. With an angle of sideslip (AOS), the secondary flow which is caused by sidewalls reduces the air-intake performance: total pressure recovery and mass capture ratio. Both theoretical and atheoretical oblique shock waves are generated on the 1st ramp. This state causes the air-intake performance deterioration. On the combustion test, heat tolerance of the thermal insulator and the ignition with the igniter are confirmed. The measured maximum combustion temperature is 1138 K. We plan to conduct a system firing test using the ramjet test facility (RJTF) in JAXA to obtain the integrated performance for the first flight experiment.

    Original languageEnglish
    Title of host publication22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
    PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
    ISBN (Print)9781624105777
    DOIs
    Publication statusPublished - 2018 Jan 1
    Event22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018 - Orlando, United States
    Duration: 2018 Sep 172018 Sep 19

    Other

    Other22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018
    CountryUnited States
    CityOrlando
    Period18/9/1718/9/19

    Fingerprint

    ramjet engines
    Ramjet engines
    Integrated control
    research and development
    Mach number
    engine
    air intakes
    Air intakes
    supersonic wind tunnels
    wind tunnel tests
    flight
    experiment
    Experiments
    heat tolerance
    Wind tunnels
    engines
    combustion
    sideslip
    test firing
    oblique shock waves

    ASJC Scopus subject areas

    • Control and Systems Engineering
    • Space and Planetary Science
    • Aerospace Engineering

    Cite this

    Wakabayashi, S., Yoshida, H., Chiga, T., Satou, T., Taguchi, H., Kojima, T., ... Tsue, M. (2018). Research and development of ramjet engine for high-mach integrated control experiment (HIMICO). In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference [AIAA 2018-5319] American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2018-5319

    Research and development of ramjet engine for high-mach integrated control experiment (HIMICO). / Wakabayashi, Sho; Yoshida, Hidekazu; Chiga, Takahiro; Satou, Tetsuya; Taguchi, Hideyuki; Kojima, Takayuki; Okamoto, Toshiki; Ikeda, Yutaka; Nakaya, Shinji; Tsue, Mitsuhiro.

    22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 2018. AIAA 2018-5319.

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

    Wakabayashi, S, Yoshida, H, Chiga, T, Satou, T, Taguchi, H, Kojima, T, Okamoto, T, Ikeda, Y, Nakaya, S & Tsue, M 2018, Research and development of ramjet engine for high-mach integrated control experiment (HIMICO). in 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference., AIAA 2018-5319, American Institute of Aeronautics and Astronautics Inc, AIAA, 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, United States, 18/9/17. https://doi.org/10.2514/6.2018-5319
    Wakabayashi S, Yoshida H, Chiga T, Satou T, Taguchi H, Kojima T et al. Research and development of ramjet engine for high-mach integrated control experiment (HIMICO). In 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA. 2018. AIAA 2018-5319 https://doi.org/10.2514/6.2018-5319
    Wakabayashi, Sho ; Yoshida, Hidekazu ; Chiga, Takahiro ; Satou, Tetsuya ; Taguchi, Hideyuki ; Kojima, Takayuki ; Okamoto, Toshiki ; Ikeda, Yutaka ; Nakaya, Shinji ; Tsue, Mitsuhiro. / Research and development of ramjet engine for high-mach integrated control experiment (HIMICO). 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 2018.
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    AU - Taguchi, Hideyuki

    AU - Kojima, Takayuki

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