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  1. Performance and Regression Rate Characteristics of 5-kN Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

    Article • Journal of Propulsion and Power, July 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Toru Shimada, Takashi Sakurai, Koki Kitagawa

  2. Fuel Regression Behavior of a Swirling-Injection End-Burning Hybrid Rocket Engine using Paraffin-based Fuels

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Takashi Sakurai

  3. Applicability of a LOx Vaporization Preburner for Swirling-Flow Hybrid Rocket Engines

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Takashi Sakurai

  4. A Fundamental Study of a End-Burning Swirling-Flow Hybrid Rocket Engine using Low Melting Temperature Fuels

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Takashi Sakurai