论文信息 - System Performance of a Microwave Discharge Miniature Ion Thruster - 字舞流文

System Performance of a Microwave Discharge Miniature Ion Thruster

Hiroyuki Koizumi | Hitoshi Kuninaka

[1] Henry Oman,et al. Fundamentals of Electric Propulsion , 2006 .

[2] Hitoshi Kuninaka,et al. Sub-Milli-Newton Class Miniature Microwave Ion Thruster , 2007 .

[3] R. Jahn,et al. Physics of Electric Propulsion , 1968 .

[4] Y. Takao,et al. Development of small scale microwave discharge ion thruster with variable magnetic field , 2004, 2012 International Conference on Renewable Energy Research and Applications (ICRERA).

[5] J. Kawaguchi,et al. The Rubble-Pile Asteroid Itokawa as Observed by Hayabusa , 2006, Science.

[7] Naoji Yamamoto,et al. Antenna Configuration Effects on Thrust Performance of Miniature Microwave Discharge Ion Engine , 2006 .

[8] Juergen Mueller,et al. Miniature Ion Thrusters for Precision Formation Flying , 2004 .

[9] D. Feili,et al. Testing of new ?N-RITs at Giessen , 2005 .

[10] K. Nishiyama,et al. Powered Flight of Electron Cyclotron Resonance Ion Engines on Hayabusa Explorer , 2007 .

[11] Hiroyuki Koizumi,et al. Antenna Design Method for Low Power Miniaturized Microwave Discharge Ion Engines , 2009 .