[B-5] Arcjets / MPD Thrusters

[2022-b-22] Performance Characteristics of High-Thrust High-specific-Impulse Steady-State Magneto-Plasma-Dynamic Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in the Planets and Satellites to Propellants-

*Ayano Yoshida¹, Ryo Ikemoto¹, Kazuki Shibutani¹, Kentaro Kaji¹, Hirokazu Tahara¹, Ai Momozawa², Daisuke Nakata³, Tomoyuki Ikeda⁴, Yoshiyuki Takao⁵, Takashi Wakizono⁶, Masaya Toyama⁷ (1. Osaka Sangyo University, Department of Mechanical Engineering , 2. Tokyo City University, 3. Muroran Institute of Technology, 4. Tokai University, 5. Nishinippon Institute of Technology, 6. High Serve, Inc., 7. Pasett, Inc.)

キーワード：Electric Propulsion, Magnetoplasmadynamic (MPD) Thruster, Applied Magnetic Field, Solar System, In-Space Propulsion