Geometric Parameter Effect of Magneto-Plasma-Dynam...-Reference-Cited by-同舟云学术

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Geometric Parameter Effect of Magneto-Plasma-Dynam...

Published:2005-10-17 Issue: Volume: Page:
ISSN:
Container-title:56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law
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Author:

Nakata Daisuke¹,Toki Kyoichiro²,Funaki Ikkoh³,Shimizu Yukio³,Kuninaka Hitoshi³,Arakawa Yoshihiro¹

Affiliation:

1. Department of Aeronautics and Astronautics, University of Tokyo 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, JAPAN

2. Tokyo University of Agriculture and Technology 2-24-16, Nakacho, Koganei-shi, Tokyo 184-8588, JAPAN

3. Institute of Space and Astronautical Science / Japan Aerospace Exploration Agency 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, JAPAN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.IAC-05-E2.P.11

Reference29 articles.

1. A Survey of Propulsion Options for Cargo and Piloted Missions to Mars

2. MPD thruster performance with various propellants

Cited by 1 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

1. The Effect of Anode Configuration on Hydrogen MPD Thruster Performance: A Numerical Study;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2018

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