[S-3] Finalist Student Session 3

[2022-b-53s] Experimental prediction of performance degradation during space operation in thrust-enhanced microwave discharge ion thruster µ10

*Kana Hattori¹, Yusuke Yamashita¹, Ryo Shirakawa², Satoshi Hosoda³, Ryudo Tsukizaki³, Kazutaka Nishiyama³ (1. The University of Tokyo. Department of Aeronautics and Astronautics, 2. Kobe University. Department of Mechanical Engineering, 3. JAXA. Institute of Space and Astronautical Science)

キーワード：Gridded ion thruster, Plasma hysteresis, Hayabusa2, Carbon contamination