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    Paper code

    IAC-17,C4,2,10,x41528

    Place

    2017-09-26 09:45, #10, Hall E3

    Title

    Throttling Capability and LOX Vaporization for Hybrid Rocket Engine with Multi-Section Swirl Injection Method

    abstract

    View PDF

    Session

    2. Propulsion System (2)

    symposium

    C4. SPACE PROPULSION SYMPOSIUM

    congress

    IAC-17

    Type of presentation

    oral

    Main author

    Prof. Shigeru Aso, Kyushu University, Japan

    Co-authors

    Dr. Yasuhiro Tani, Kyushu University, Japan;

    Mr. Masato Yamashita, Kyushu University, Japan;

    Mr. Satoru Komori, Kyushu University, Japan;

    Mr. Tomohiro Yamasaki, Kyushu University, Japan;

    Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;