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  1. 030 理工学 Science & engineering
  2. 学術雑誌掲載論文

Direct thrust measurements and modelling of a radio-frequency expanding plasma thruster

https://iwate-u.repo.nii.ac.jp/records/10095
https://iwate-u.repo.nii.ac.jp/records/10095
4aa1e09b-45d2-4d5e-a9d7-c4da2d4b4195
名前 / ファイル ライセンス アクション
pp-v18i8p080701.pdf pp-v18i8p080701.pdf (342.0 kB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2011-11-04
タイトル
タイトル Direct thrust measurements and modelling of a radio-frequency expanding plasma thruster
キーワード
主題Scheme Other
主題 plasma devices
キーワード
主題Scheme Other
主題 plasma diagnostics
キーワード
主題Scheme Other
主題 plasma magnetohydrodynamics
キーワード
主題Scheme Other
主題 plasma pressure
キーワード
主題Scheme Other
主題 plasma transport processes
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ journal article
著者 Lafleur, T

× Lafleur, T

Lafleur, T

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Takahashi, K

× Takahashi, K

Takahashi, K

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Charles, C

× Charles, C

Charles, C

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Boswell, R. W.

× Boswell, R. W.

Boswell, R. W.

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著者(機関)
値 Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering, The Australian National University
著者(機関)
値 Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering, The Australian National University, Department of Electrical Engineering and Computer Science, Iwate University
著者(機関)
値 Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering, The Australian National University
著者(機関)
値 Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering, The Australian National University
登録日
日付 2011-11-04
書誌情報 Physics of Plasmas

巻 18, 号 8, p. 080701-1-080701-4, 発行日 2011-01-01
ISSN
収録物識別子タイプ ISSN
収録物識別子 1070-664X
Abstract
内容記述タイプ Other
内容記述 It is shown analytically that the thrust from a simple plasma thruster (in the absence of a magnetic field) is given by the maximum upstream electron pressure, even if the plasma diverges downstream. Direct thrust measurements of a thruster are then performed using a pendulum thrust balance and a laser displacement sensor. A maximum thrust of about 2 mN is obtained at 700 W for a thruster length of 17.5 cm and a flow rate of 0.9 mg s−1, while a larger thrust of 4 mN is obtained at a similar power for a length of 9.5 cm and a flow rate of 1.65 mg s−1. The measured thrusts are in good agreement with the maximum upstream electron pressure found from measurements of the plasma parameters and in fair agreement with a simple global approach used to model the thruster.
出版者
出版者 American Institute of Physics
権利
権利情報 (C) 2011 American Institute of Physics
権利
権利情報 Copyright 2011 American Institute of Physics. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the American Institute of Physics.
DOI
関連タイプ isIdenticalTo
識別子タイプ DOI
関連識別子 10.1063/1.3610570
著者版フラグ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
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