The Effect of Anode Configuration on Hydrogen MPD Thruster Performance: A Numerical Study-Reference-Cited by-同舟云学术

The Effect of Anode Configuration on Hydrogen MPD Thruster Performance: A Numerical Study

Published:2018 Issue:3 Volume:16 Page:274-279
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:

TAUCHI Shitan¹,KAWASAKI Akira²,NAKANE Masakatsu³,KUBOTA Kenichi⁴,FUNAKI Ikkoh⁵

Affiliation:

1. Department of Space and Astronautical Science, SOKENDAI (The Graduate University for Advanced Studies)

2. Department of Aerospace Engineering, Nagoya University

3. Department of Aerospace Engineering, Nihon University

4. Aeronautical Technology Directorate, JAXA

5. Institute of Space and Astronautical Science, JAXA

Publisher

Japan Society for Aeronautical and Space Sciences

Link

Reference17 articles.

1. 1) ISECG: The Global Exploration Roadmap, NASA, 2013

2. 2) Kuriki, K. and Arakawa, Y.: Introduction to Electric Propulsion, University of Tokyo Press, 2003, pp. 119-139 (in Japanese).

5. 5) Malliaris, A. C. and Libby, D. R.: Spectroscopic study of ion-neutral coupling in plasma acceleration, AIAA J., 9 (1970), pp. 160-168.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献