Numerical Investigation of Neutral-Injection Effect on an Electrodeless Plasma Thruster-Reference-Cited by-同舟云学术

Numerical Investigation of Neutral-Injection Effect on an Electrodeless Plasma Thruster

Published:2018 Issue:2 Volume:16 Page:105-109
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:

TAKASE Kazuki¹,TAKAHASHI Kazunori²,TAKAO Yoshinori³

Affiliation:

1. Department of Systems Integration, Yokohama National University

2. Department of Electrical Engineering, Tohoku University

3. Division of Systems Research, Yokohama National University

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/16/2/16_105/_pdf

Reference17 articles.

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3. 3) Chen, F. F.: Helicon Discharges and Sources: A Review, Plasma Sources Sci. Technol., 24 (2015), pp. 014001-1-014001-25.

4. 4) Charles, C.: A Review of Recent Laboratory Double Layer Experiments, Plasma Sources Sci. Technol., 16 (2007), pp. R1-R25.

5. 5) Squire, J. P., Olsen, C. S., Chang Diaz, F. R., Cassady, L. D., Longmier, B. W., Ballenger, M. G., Carter, M. D., Glover, T. W., and McCaskill, G. E.: VASIMR VX-200 Operation at 200 kW and Plume Measurements: Future Plans and an ISS EP Test Platform, Proceedings of the 32nd International Electric Propulsion Conference, Wiesbaden, Germany, 2011, IEPC-2011-154.