All Stories

  1. Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant

    Article • Journal of Propulsion and Power, November 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Akira Ando, Yoshinori Takao

  2. Characterization of Helicon Plasma Thruster Performance Operated for Various Rare Gas Propellants

    Article • Journal of Propulsion and Power, May 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Atsushi Komuro, Prof. Akira Ando

  3. High-power, low-pressure, inductively coupled RF plasma source using a FET-based inverter power supply

    Article • Japanese Journal of Applied Physics, December 2014, Japan Society of Applied Physics

    Prof. Akira Ando