16:20 〜 16:40
[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.)
キーワード：Arcjet Thruster, Alternative Propellant, Carbon Dioxide, Methane, Solar System