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Verification of a Charging Potential Measurement Method using a Parallel Plate Electrostatic Analyzer
http://hdl.handle.net/10228/00006152
http://hdl.handle.net/10228/00006152404e23dd-f797-4f98-8924-eec67d592b94
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
TTJS-8-1-7.pdf (689.9 kB)
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| Item type | 学術雑誌論文 = Journal Article(1) | |||||
|---|---|---|---|---|---|---|
| 公開日 | 2017-04-19 | |||||
| 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 | |||||
| タイトル | ||||||
| タイトル | Verification of a Charging Potential Measurement Method using a Parallel Plate Electrostatic Analyzer | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 著者 |
Kurahara, Naomi
× Kurahara, Naomi× 趙, 孟佑 |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | The analysis and evaluation of spacecraft charging are important tasks related to spacecraft design. Plasma parameters and charging potential data are needed for charging and discharging predictions. A new type of electrostatic analyzer using two-stage parallel electrodes has been developed to measure the charging potential of a spacecraft over a wide range, from one volt to tens of kilovolts. The spacecraft charging potential is determined by analyzing the energy spectrum shift. A proof-of-concept model of the new electrostatic analyzer was tested in a vacuum chamber filled with Xe plasma. The experimental results agreed very well with the theoretical predictions. The device, made of two parallel plate electrodes, can measure the charging potential by scanning the electrode voltage over only one-tenth of the actual charging potential. The simple structure and low-voltage operation make the device suitable for operation on a small satellite. | |||||
| 言語 | en | |||||
| 書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 8, p. 1-7, 発行日 2010-04 |
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| 出版社 | ||||||
| 出版者 | 日本航空宇宙学会 | |||||
| 言語 | ja | |||||
| DOI | ||||||
| 関連タイプ | isIdenticalTo | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | https://doi.org/10.2322/tastj.8.1 | |||||
| NCID | ||||||
| 収録物識別子タイプ | NCID | |||||
| 収録物識別子 | AA0086707X | |||||
| ISSN | ||||||
| 収録物識別子タイプ | PISSN | |||||
| 収録物識別子 | 0549-3811 | |||||
| ISSN | ||||||
| 収録物識別子タイプ | EISSN | |||||
| 収録物識別子 | 1884-0485 | |||||
| 著作権関連情報 | ||||||
| 権利情報 | Copyright (c) 2010 The Japan Society for Aeronautical and Space Sciences | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Spacecraft Charging | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Langmuir Probe | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Electrostatic Analyzer | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Plasma Measurement | |||||
| 出版タイプ | ||||||
| 出版タイプ | VoR | |||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
| 査読の有無 | ||||||
| 値 | yes | |||||
| 研究者情報 | ||||||
| URL | https://hyokadb02.jimu.kyutech.ac.jp/html/168_ja.html | |||||
| 論文ID（連携） | ||||||
| 値 | 10017556 | |||||
| 連携ID | ||||||
| 値 | 516 | |||||
