| アイテムタイプ |
学術雑誌論文 / Journal Article(1) |
| 公開日 |
2011-11-02 |
| タイトル |
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|
タイトル |
Direct thrust measurement of a permanent magnet helicon double layer thruster |
| キーワード |
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|
主題Scheme |
Other |
|
主題 |
argon |
| キーワード |
|
|
主題Scheme |
Other |
|
主題 |
ion engines |
| キーワード |
|
|
主題Scheme |
Other |
|
主題 |
plasma density |
| キーワード |
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|
主題Scheme |
Other |
|
主題 |
plasma devices |
| キーワード |
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|
主題Scheme |
Other |
|
主題 |
plasma diagnostics |
| 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 sheaths |
| 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 |
Takahashi, K
Lafleur, T
Charles, C
Alexander, P
Boswell, R.W
Perren, M
Laine, R
Pottinger, S
Lappas, V
Harle, T
Lamprou, D
|
| 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) |
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|
値 |
Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering,The Australian National University |
| 著者(機関) |
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|
値 |
Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering,The Australian National University |
| 著者(機関) |
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|
値 |
Space Plasma, Power and Propulsion Group, Research School of Physics and Engineering,The Australian National University |
| 著者(機関) |
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|
値 |
ASTRIUM-EADS |
| 著者(機関) |
|
|
値 |
ASTRIUM-EADS |
| 著者(機関) |
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|
値 |
Surrey Space Centre, University of Surrey |
| 著者(機関) |
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|
値 |
Surrey Space Centre, University of Surrey |
| 著者(機関) |
|
|
値 |
Surrey Space Centre, University of Surrey |
| 著者(機関) |
|
|
値 |
Surrey Space Centre, University of Surrey |
| 登録日 |
|
|
日付 |
2011-11-02 |
| 書誌情報 |
Applied Physics Letters
巻 98,
号 14,
p. 141503-1-141503-3,
発行日 2011-01-01
|
| ISSN |
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収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0003-6951 |
| Abstract |
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|
内容記述タイプ |
Other |
|
内容記述 |
Direct thrust measurements of a permanent magnet helicon double layer thruster have been made using a pendulum thrust balance and a high sensitivity laser displacement sensor. At the low pressures used (0.08 Pa) an ion beam is detected downstream of the thruster exit, and a maximum thrust force of about 3 mN is measured for argon with an rf input power of about 700 W. The measured thrust is proportional to the upstream plasma density and is in good agreement with the theoretical thrust based on the maximum upstream electron pressure. |
| 出版者 |
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|
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 |
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|
関連タイプ |
isIdenticalTo |
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|
識別子タイプ |
DOI |
|
|
関連識別子 |
10.1063/1.3577608 |
| 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 |
apl-v98n14p141503.pdf (110.6 kB)
