[B-5] Arcjets / MPD Thrusters

[2022-b-21] Performance Characteristics of DC Arcjet Thrusters -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in Planets and Satellites in the Solar System to Propellants-

*Kentaro Kaji¹, Kazuki Shibutani¹, Ryo Ikemoto¹, Ayano Yoshida¹, 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, Inc., 7. High Serve, Inc., 8. Pasett, Inc.)

キーワード：Arcjet Thruster, Attitude Control, Orbital Transportation, Solar System, Carbon Dioxide