Transient Behavior of Ion Extraction and Acceleration of Variable Thrust Ion Thruster

Author:

NAKANO Masakatsu1,YAMAMOTO Naoji2,FUNAKI Ikkoh3,OHKAWA Yasushi4

Affiliation:

1. Tokyo Metropolitan College of Industrial Technology

2. Kyushu University

3. Institute of Space and Astronautical Science, JAXA

4. Research and Development Directorate, JAXA

Publisher

Japan Society for Aeronautical and Space Sciences

Reference18 articles.

1. 1) Arakawa, Y., Kuninaka, H., Nakayama, Y., and Nishiyama, K.: Ion Engines for Powered Flight in Space, Corona Publishing Co., LTD., Tokyo, 2006, pp. 10–12 (in Japanase).

2. 2) Kawahara, Y., Yamamoto, N., Funaki, I., Morita, D., Ohkawa, Y., Takamatsu, I., Nakano, M., and Iijima, K.: Feasibility Study on On/Off Control of Ion Engines, STEP-2016-035, Proceedings of Space Transportation Symposium, 2017 (in Japanese).

3. 3) Nakano, M., Yamamoto, N., Funaki, I., and Ohkawa, Y.: Transient Simulation of Ion Beam Extraction for On-Off Control, STEP-2016-034, Proceedings of Space Transportation Symposium, 2017 (in Japanase).

4. 4) Gamero-Castano, M., Hruby, V., Spence, D., Demmons, N., McCormik, R., Gasdaska, C., and Falkos, P.: Micro Newton Colloid Thruster System Development for ST7-DRS Mission, AIAA Paper 2003-4543, 2003.

5. 5) Hruby, V., Spence, D., Demmons, N., Roy, T., Ehrbar, E., Zwahlen, J., Martin, R., Ziemer, J., Randolph, T., Connolly, W., Rhodes, S., and Tolman, W.: ST7-DRS Colloid Thruster System Development and Performance Summary, AIAA Paper 2008-4824, 2008.

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