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  1. Combustion Characteristics of Stabilized Combustion with Liquid Oxygen Under High Pressure Conditions

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Mai Fukada, Harunori Nagata, Kaii Ri, Mao Yamaguchi

  2. The Analytical Study for Operation Condition of Axial-Injection End-Burning Hybrid Rocket

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Mai Fukada, Harunori Nagata, Kaii Ri

  3. Experimental and Numerical Investigation on the Regression to Spread Transition Mechanism in Axial-Injection End-Burning Hybrid Rocket Motor

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Mai Fukada

  4. Obtaining C* Efficiency and Establishing Ignition Sequences in Axial-Injection-End-Burning Hybrid Rockets (AIEB-HR) Using Liquid Oxygen

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Mai Fukada, Harunori Nagata, Kaii Ri

  5. Combustion Characteristics of Stabilized Combustion with Liquid Oxygen at Different Operating Conditions

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Masashi Wakita, Harunori Nagata, Kaii Ri, Mai Fukada