[b-2] Alternative Propellant for Ion Thruster

[2023-b-05] Thrust performance of ion thrusters with nitrogen propellant

*Ryotaro Matsumoto¹, Ryo Shiraki¹, Naoji Yamamoto¹, Masakatsu Nakano² (1. Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, Japan, 2. Tokyo Metropolitan College of Industrial Technology, Japan)

キーワード：ion thruster, nitrogen, alternative propellant, specific impulse