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Space Dust Impacts Detector Development for the Evaluation of Ejecta
http://hdl.handle.net/10228/00007225
http://hdl.handle.net/10228/00007225a417bb5f-d2ce-44a2-83e0-9ea1eec9c1d4
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2018_add02.pdf (1.7 MB)
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| Item type | 会議発表論文 = Conference Paper(1) | |||||||||||
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| 公開日 | 2019-06-18 | |||||||||||
| 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 | Space Dust Impacts Detector Development for the Evaluation of Ejecta | |||||||||||
| 言語 | en | |||||||||||
| 言語 | ||||||||||||
| 言語 | eng | |||||||||||
| 著者 |
Faure, Pauline
× Faure, Pauline× Masuyama, Shingo× Nakamoto, Hiroshi× 赤星, 保浩
WEKO
5459
× Kitazawa, Yukihito× Koura, Takao |
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| 抄録 | ||||||||||||
| 内容記述タイプ | Abstract | |||||||||||
| 内容記述 | This paper aims at a) introducing the space dust impacts detector developed at Kyushu Institute of Technology (KIT), b) presenting the detector utility for the evaluation of ejecta, and c) raising awareness of the space community regarding the risk represented by orbital debris. The space dust impacts detector introduced into this paper belongs to the in-situ detection systems and has for purposes to be a) light, 30 g, b) low cost, about EUR200, c) low power consuming, 0.01W, d) easily adaptable on-board of spacecraft, and e) able to detect impacts of debris with a diameter ranging from 100 μm to 600 μm. The detector is mounted on the nano-satellite, Horyu-II, developed at KIT and launched on May 18, 2012. The data received will be very helpful to identify the detector's strengths and weaknesses to improve it and create a second version that will aim at evaluating ejecta fragments produced during hypervelocity impact testing. An accurate evaluation of ejecta is critical for orbital debris risk assessment and mitigation. If all space activities were stopped, debris will still be created by chain reaction. The number of debris could then become so large, that the access to certain LEOs will be quasi-impossible, which will jeopardize the space exploration as well as scientific, educational, and security missions that benefit to all mankind. Debris is therefore a serious issue that should be taken into consideration at every step of the development of a small or large spacecraft. | |||||||||||
| 備考 | ||||||||||||
| 内容記述タイプ | Other | |||||||||||
| 内容記述 | 2012 Hypervelocity Impact Symposium (HVIS 2012), September 16-20, 2012, Baltimore, Maryland | |||||||||||
| 書誌情報 |
Procedia Engineering 巻 58, p. 594-600, 発行日 2012-09 |
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| 出版社 | ||||||||||||
| 出版社 | Elsevier | |||||||||||
| DOI | ||||||||||||
| 関連タイプ | isIdenticalTo | |||||||||||
| 識別子タイプ | DOI | |||||||||||
| 関連識別子 | https://doi.org/10.1016/j.proeng.2013.05.068 | |||||||||||
| ISSN | ||||||||||||
| 収録物識別子タイプ | EISSN | |||||||||||
| 収録物識別子 | 1877-7058 | |||||||||||
| 著作権関連情報 | ||||||||||||
| 権利情報 | Copyright (c) 2013 The Authors. Published by Elsevier Ltd. Open access under CC BY-NC-ND license. | |||||||||||
| 著作権関連情報 | ||||||||||||
| 権利情報 | http://creativecommons.org/licenses/by-nc-nd/3.0/ | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Space environment | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Debris | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Hypervelocity impact | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Modeling | |||||||||||
| 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 | 7726 | |||||||||||
