Design of High Efficiency Grid System for Water Propellant Miniature Ion Thrusters-Reference-Cited by-同舟云学术

Design of High Efficiency Grid System for Water Propellant Miniature Ion Thrusters

Published:2020 Issue:6 Volume:18 Page:412-416
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

NAKANO Masakatsu¹,NAKAMURA Kengo²,NAKAGAWA Yuichi³,TAKAO Yoshinori²,KOIZUMI Hiroyuki³

Affiliation:

1. The Tokyo Metropolitan College of Industrial Technology

2. Yokohama National University

3. The University of Tokyo

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/18/6/18_18.412/_pdf

Reference15 articles.

1. 1) Arakawa, Y., Kuninaka, H., Nakayama, N., and Nishiyama, K.: Ion Engines for Powered Flight in Space, Corona Publishing, Tokyo, 2006, pp. 18–20 (in Japanese).

2. 2) Casaregola, C.: Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platforms, 34th International Electric Propulsion Conference, Kobe, Japan, IEPC-2015-97, 2015.

3. 3) Corbett, M. H. and Edwards, C. H.: Thrust Control Algorithms for the GOCE Ion Propulsion Assembly, 30th International Electric Propulsion Conference, Florence, Italy, IEPC-2007-210, 2007.

4. 4) 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.

5. 5) Garner, C. E., Rayman, M. D., and Brophy, J.: In-Flight Operation of the Dawn Ion Propulsion System-Arrival at Ceres, 34th International Electric Propulsion Conference, Kobe, Japan, IEPC-2015-88, 2015.

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