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Development of Low Cost Double Probe Plasma Measurement System for a Lean Satellite HORYU-IV
http://hdl.handle.net/10228/00007276
http://hdl.handle.net/10228/00007276b91937be-e61c-4417-8533-c9cf6daeb9b4
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2016_09.pdf (1.0 MB)
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| アイテムタイプ | 会議発表論文 = Conference Paper(1) | |||||
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| 公開日 | 2019-07-04 | |||||
| 資源タイプ | ||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
| 資源タイプ | conference paper | |||||
| タイトル | ||||||
| タイトル | Development of Low Cost Double Probe Plasma Measurement System for a Lean Satellite HORYU-IV | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | jpn | |||||
| 著者 |
Tejumola, Taiwo R.
× Tejumola, Taiwo R.× Tanaka, Atomu× Khan, Arifur× HORYU-IV Project Team× 趙, 孟佑 |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | A lean satellite is equivalent to a small/micro/nano/pico satellite that utilizes untraditional risk-taking development approaches to achieve low-cost and fast-delivery. Lean satellites have demonstrated great ability to be used for the study of space plasma and Earth’s ionosphere which has helped in the prediction of many astrophysical phenomena and forecasting of geophysical changes on ground. Several methods have been employed in the measurement of space plasma parameters over the years using the Langmuir Probe. These methods employed different techniques using single probes or double probes. Single probe requires a well-defined reference which is difficult in small spacecraft. Moreover, high current flow in the saturation mode may destroy the probe and on-board circuitry. A low cost double Langmuir probe made of gold with its measurement circuit has been designed and tested inside RF generated Argon plasma in the pressure of 1.4×10-2 Pa that confirms the electron density from 1010 to 1012 m-3. Important design considerations such as operability of the designed system in low earth orbit grade plasma, mitigation of probe contamination and sputtering of the electrode surface were analysed in the paper to ensure that the developed system can provide high fidelity plasma measurement data throughout the life span of HORYU-IV (Arc Event Generator and Investigator Satellite) which is a 13 kg, 40 cm cubic lean satellite under development at the Kyushu Institute of Technology. | |||||
| 言語 | en | |||||
| 備考 | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | 30th International Symposium on Space Technology and Science (ISTS), July 4th-July 10th, 2015, Kobe-Hyogo, Japan | |||||
| 書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 14, 号 ists30, p. Pr_39-Pr_46, 発行日 2015-07-09 |
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| 出版社 | ||||||
| 出版社 | 日本航空宇宙学会 | |||||
| 言語 | en | |||||
| 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.14.Pr_39 | |||||
| CRID | ||||||
| 関連タイプ | isIdenticalTo | |||||
| 識別子タイプ | URI | |||||
| 関連識別子 | https://cir.nii.ac.jp/crid/1390001205321298432 | |||||
| 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) 2016 by the Japan Society for Aeronautical and Space Sciences and ISTS. | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Plasma | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Double Langmuir Probe | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | HORYU-IV | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Contamination | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Lean Satellite | |||||
| 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 | |||||
| 連携ID | ||||||
| 値 | 7712 | |||||
