Influences of cathode position on operations and thrust performance of side by side Hall thruster system

Author:

Miyasaka Takeshi,Kita Tomohiro,Asahara Makoto,Oishi Kazuya,Sakoda Masahiro,Mamiya Yuki,Kanie Hiroki

Funder

JSPS KAKENHI

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation

Reference26 articles.

1. Overview on developments of high-power anode layer thruster in Japan;Miyasaka,2013

2. Takegahara, H., Kuninaka, H., Funaki, I., Ando, A., Komurasaki, K., Koizumi, H., Schönherr, T., Shinohara, S., Tanikawa, T., Nakano, M., Nakayama, Y., Sasoh, A, Miyasaka, T., Tahara, H., Yamamoto, N., Kakami, A., “Overview of Electric Propulsion Research Activities in Japan.

3. Low- cost 20 kW Hall thruster for mass transportation;Schönherr,2012

4. Discharge plasma fluctuations Hall thrusters;Yamamoto;Vacuum,2002

5. Yamamoto, N., Ezaki, T. and Nakashima, H., “Thrust performance of a low power Hall thruster,” Trans. of Japan Soc. for Aeronautical and Space Sci., Aerospace Technology Japan [online journal], Vol. 10, No. ists 28, URL: https://www.jstage.jst.go.jp/browse/tastj [cited 9 March 2011].

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