WEKO3
アイテム
Feasibility of Standardized Ejecta Evaluation for Spacecraft Surface Materials
http://hdl.handle.net/10228/00007226
http://hdl.handle.net/10228/00007226d6767990-7c5d-4b97-aabf-c949d00d36cd
| 名前 / ファイル | ライセンス | アクション |
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LaSEINE-2018_add01.pdf (1.7 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 | 2019-06-18 | |||||||||||
| 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 | Feasibility of Standardized Ejecta Evaluation for Spacecraft Surface Materials | |||||||||||
| 言語 | en | |||||||||||
| 言語 | ||||||||||||
| 言語 | eng | |||||||||||
| 著者 |
Masuyama, Shingo
× Masuyama, Shingo× Matsumoto, Shie× Faure, Pauline× Nakamoto, Hiroshi× 赤星, 保浩
WEKO
5459
× Koura, Takao× Matsumoto, Haruhisa× Kitazawa, Yukihito |
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| 抄録 | ||||||||||||
| 内容記述タイプ | Abstract | |||||||||||
| 内容記述 | Although a large spacecraft such as the International Space Station and other artificial satellites are thriving in the space environment due to the remarkable progress in the space development sector, their collisions with space debris are a growing concern. To examine the impact proof performance of spacecraft to space debris, hypervelocity impact experiments using a two-stage light gas gun and so on are necessary. However, space debris impact experiments are conducted in different manners dependent on the countries and the facilities. Therefore direct comparisons of the experimental results among different facilities are often difficult from the same viewpoint. In this study, the authors aim at assessment of international standardization of the hypervelocity impact experiments procedure. Projectiles with a diameter of 1 mm were used to simulate space debris impacting a target at 5 km/s. Copper witness plates were used to catch the secondary debris, namely ejecta, generated during the experiments. The size distributions of diameter of craters made by ejecta were measured on the witness plates, and they are compared one another among a solar array coupon, CFRP honeycomb and Aluminum honeycomb. | |||||||||||
| 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. 543-549, 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.2013.05.062 | |||||||||||
| 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 debris | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Two-stage light gas gun | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Ejecta | |||||||||||
| キーワード | ||||||||||||
| 主題Scheme | Other | |||||||||||
| 主題 | Hypervelocity impact | |||||||||||
| 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 | 7725 | |||||||||||
