All Stories

  1. Fuel Regression Characteristics of CAMUI-Type Hybrid Rocket with Hydrogen Peroxide

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

    Masashi Wakita, Harunori Nagata

  2. Application of Preheated Low-concentration Hydrogen Peroxide as an Oxidizer for Hybrid Rockets

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

    Masashi Wakita, Harunori Nagata

  3. 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

  4. Application of Low Concentration Hydrogen Peroxide for Hybrid Rocket Propulsion System for Small Spacecraft

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Masashi Wakita, Harunori Nagata

  5. Initial Firing Tests of Aluminum Rod/Water Hybrid Rockets

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

    Landon Kamps, Masashi Wakita, Harunori Nagata, Ayumu Tsuji

  6. Preliminary Thermal Design for Microsatellites Deployed from International Space Station’s Kibo Module

    Article • Journal of Thermophysics and Heat Transfer, July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Harunori Nagata, Masashi Wakita

  7. Fuel Regression Characteristics of a Novel Axial-Injection End-Burning Hybrid Rocket

    Article • Journal of Propulsion and Power, January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Masashi Wakita, Harunori Nagata

  8. Verification Firings of End-Burning Type Hybrid Rockets

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

    Masashi Wakita, Harunori Nagata

  9. Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets

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

    Landon Kamps, Masashi Wakita, Harunori Nagata

  10. Experimental and Analytical Investigation of Effect of Pressure on Regression Rate of Axial-Injection End-Burning Hybrid Rockets

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

    Masashi Wakita, Harunori Nagata

  11. Verification Firings of End-burning Type Hybrid Rockets

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

    Masashi Wakita, Harunori Nagata

  12. Thermal Design Procedure for Micro- and Nanosatellites Pointing to Earth

    Article • Journal of Thermophysics and Heat Transfer, July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Mr Tilok Kumar Das, Ryota Inoue, Masashi Wakita, Harunori Nagata