Numerical Investigation of Discharge Current Path in a Hydrogen MPD Thruster-Reference-Cited by-同舟云学术

Numerical Investigation of Discharge Current Path in a Hydrogen MPD Thruster

Published:2016 Issue:3 Volume:136 Page:141-146
ISSN:0385-4205
Container-title:IEEJ Transactions on Fundamentals and Materials
language:en
Short-container-title:IEEJ Trans. FM

Author:

Kawasaki Akira¹,Kubota Kenichi²,Funaki Ikkoh²,Okuno Yoshihiro¹

Affiliation:

1. Department of Energy Sciences, Tokyo Institute of Technology

2. Japan Aerospace Exploration Agency

Publisher

Institute of Electrical Engineers of Japan (IEE Japan)

Subject

Electrical and Electronic Engineering

Link

https://www.jstage.jst.go.jp/article/ieejfms/136/3/136_141/_pdf

Reference18 articles.

1. (1) K. Kuriki and Y. Arakawa : Introduction to Electric Propulsion, Univ. Tokyo Press, Tokyo (2003) (in Japanese)

2. (2) K. Uematsu, S. Morimoto, and K. Kuriki : “MPD Thruster Performance with Various Propellants”, J. Spacecraft, Vol. 22, No. 4, pp. 412-416 (1982)

3. (3) J. S. Sovey and M. A. Mantenieks : “Performance and Lifetime Assessment of Magnetoplasmadynamic Arc Thruster Technology”, J. Propul., Vol. 7, No. 1, pp. 71-83 (1991)

4. (4) H. Tahara, Y. Kagaya, and T. Yoshikawa : “Arc Structure in a Quasi-Steady MPD Thruster”, J. JSASS, Vol. 33, No. 382, pp. 42-50 (1985) (in Japanese)

5. (5) I. Funaki, K. Toki, and K. Kuriki : “Electrode Configuration Effect on the Performance of a Two-Dimensional Magnetoplasmadynamic Arcjet”, J. Propul. Power, Vol. 14, No. 6, pp. 1043-1048 (1998)

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