[b-10] Resistojet, Arcjet & MPD Thrusters

[2023-b-37] Performance Characteristics and Their Enhancement of Steady-State MPD Thrusters with Permanent Magnets 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, Yuta Nanri¹, Daiki Mori¹, 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, Ltd., 7. Pasett, Ltd.)

Keywords:Magneto-Plasma-Dynamic (MPD) Thruster, Permanent Magnet, Alternative Propellant, Carbon Dioxide, Methane