[b-10] Resistojet, Arcjet & MPD Thrusters

[2023-b-36] Performance Characteristics and Their Enhancement of Direct-Current Arcjet Thrusters -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Ice/Water etc. in Planets and Satellites in the Solar System to Propellants-

*Ryo Ikemoto¹, Yui Sasai¹, Fuma Furutani¹, Hirokazu Tahara¹, Ai Momozawa², Daisuke Nakata³, Tomoyuki Ikeda⁴, Yoshiyuki Takao⁵, Yuichiro Nogawa⁶, Takashi Wakizono⁷, Masaya Toyama⁸ (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. Splije, Ltd., 7. High Serve, Ltd., 8. Pasett, Ltd.)

Keywords:Arcjet Thruster, Alternative Propellant, Carbon Dioxide, Methane, Solar System