Nozzle Shape Optimization for an MPD Thruster Using a Two-Dimensional Axisymmetric Flow Model-Reference-Cited by-同舟云学术

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Nozzle Shape Optimization for an MPD Thruster Using a Two-Dimensional Axisymmetric Flow Model

Published:2011 Issue:687 Volume:59 Page:90-96
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

NAKANE Masakatsu,NAGAO Masao,ISHIKAWA Yoshio,KUBOTA Kenichi,FUNAKI Ikkou

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/59/687/59_687_90/_pdf

Reference11 articles.

1. Optimal Control of Quasi-One-Dimensional Self-Field Magnetoplasmadynamic Arcjet Flowfields

2. ESD Ground Testing of Triple-Junction Space Solar Cells with Monolithic Diodes

3. 3) Nakata, D.: Discharge Pattern and Energy Balance in an MPD Thruster, Ph. D. Thesis, The University of Tokyo, 2008.

4. 4) 栗木恭一,荒川義博:電気推進ロケット入門,東京大学出版会,東京,2003.

5. Numerical Study of Plasma Behavior in a Magnetoplasmadynamic Thruster Around Critical Current

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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