All Stories

  1. Experimental Study on 5 kN Thrust Level Hybrid Rocket Motor Using the Low-Melting-Point Thermoplastic Fuel

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Yutaka Wada, Takafumi Matsui

  2. Conceptual Study on High-altitude Balloon Launch of Low Melting Point Thermoplastic Fuel/N2O Hybrid Rocket

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Yutaka Wada, Dr. Tadayoshi Shoyama, Takafumi Matsui

  3. Static Burning Tests on a Bread Board Model of Altering-intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

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

    Dr. Toru Shimada, Dr Yutaka Wada, Koki Kitagawa