Numerical Analysis of a Miniature Microwave-discharge Ion Thruster Using Water as the Propellant-Reference-Cited by-同舟云学术

Numerical Analysis of a Miniature Microwave-discharge Ion Thruster Using Water as the Propellant

Published:2018 Issue:4 Volume:61 Page:152-159
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

NAKAMURA Kengo¹,NAKAGAWA Yuichi²,KOIZUMI Hiroyuki³,TAKAO Yoshinori⁴

Affiliation:

1. Department of Systems Integration, Yokohama National University

2. Department of Aeronautics and Astronautics, The University of Tokyo

3. Department of Advanced Energy, The University of Tokyo

4. Division of Systems Research, Yokohama National University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/61/4/61_T-17-66/_pdf

Reference19 articles.

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2. 2) Koizumi, H., Kawahara, H., Yaginuma, K., Asakawa, J., Nakagawa, Y., Nakamura, Y., Kojima, S., Matsuguma, T., Funase, R., Nakatsuka, J., and Komurasaki, K.: Initial Flight Operations of the Miniature Propulsion System Installed on Small Space Probe: PROCYON, Trans. JSASS Aerospace Technology Japan, 14 (2016), pp. Pb_13–Pb_22.

3. 3) Kuninaka, H., Nishiyama, K., Funaki, I., Yamada, T., Shimizu, Y., and Kawaguchi, J.: Powered Flight of Electron Cyclotron Resonance Ion Engines on Hayabusa Explorer, J. Propul. Power, 23 (2007), pp. 544–551.

4. 4) Kuninaka, H. and Satori, S.: Development and Demonstration of a Cathodeless Electron Cyclotron Resonance Ion Thruster, J. Propul. Power, 14 (1998), pp. 1022–1026.

5. 5) Koizumi, H. and Kuninaka, H.: Miniature Microwave Discharge Ion Thruster Driven by 1 Watt Microwave Power, J. Propul. Power, 26 (2010), pp. 601–604.

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