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  • IAC-19/C4/IP
  • Paper #53776
  • Paper information

    Paper code

    IAC-19,C4,IP,34,x53776

    Order

    34

    Room

    IP Area

    Title

    The Effect of fuel length on the regression rate in swirling-oxidizer-flow-type hybrid rocket using a liquefying fuel

    abstract

    View PDF

    Session

    IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    symposium

    C4. IAF SPACE PROPULSION SYMPOSIUM

    congress

    IAC-19

    Type of presentation

    interactive

    Main author

    Mr. Yo Kawabata, Chiba Institute of Technology, Japan

    Co-authors

    Mr. Kazunari Onagano, Chiba Institute of Technology, Japan;

    Dr. Yutaka Wada, Chiba Institute of Technology, Japan;

    Mr. Nobuji Kato, Katazen Corporation, Japan;

    Prof. Keiichi Hori, Japan Aerospace Exploration Agency (JAXA), Japan;

    Prof. Ryo Nagase, Chiba Institute of Technology, Japan;