WEKO3
アイテム
Hypervelocity Impact Tests on Ejecta and its International Stabdarization
http://hdl.handle.net/10228/00007493
http://hdl.handle.net/10228/000074938b6c5bfa-94c3-4bb5-b428-6bd3378950b3
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2012_16.pdf (1.9 MB)
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| アイテムタイプ | 学術雑誌論文 = Journal Article(1) | |||||||||||||
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| 公開日 | 2019-12-12 | |||||||||||||
| 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 | Hypervelocity Impact Tests on Ejecta and its International Stabdarization | |||||||||||||
| 言語 | en | |||||||||||||
| 言語 | ||||||||||||||
| 言語 | eng | |||||||||||||
| 著者 |
赤星, 保浩
× 赤星, 保浩
WEKO
5459
× Faure, Pauline× 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 arelaunched in the earth orbit thanks to the remarkable progress in the space development, their collisions with orbital debris are an increasing concern. To examine the impact protection performance of spacecraft against orbital debris, hypervelocity impact experiments using a two-stage light gas gun and so on are necessary. There has been an active facility cross calibration program between space agencies, where tests were performed using identical targets and test conditions for each pair of tests, to assure that the results were comparable. Six distinct facility cross calibration testing campaigns have been performed between NASA and gun ranges in Germany, Russia, Japan, France, China and Canada. The test conditions for individual campaigns were negotiated at different times, so the target configuration varied between different campaigns. Projectiles with a diameter of 1 mm were used to simulate orbital debris impacting a target at velocity of 5 km/s. Copper witness plates were used as witness plates to catch the secondary debris, namely ejecta, generated due to hypervelocity impacts. 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 in this study. | |||||||||||||
| 言語 | en | |||||||||||||
| 書誌情報 |
en : The Journal of Space Technology and Science: a publication of Japanese Rocket Society 巻 26, 号 2, p. 2_48-2_55, 発行日 2012 |
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| 出版社 | ||||||||||||||
| 出版者 | 日本ロケット協会 | |||||||||||||
| 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/10.11230/jsts.26.2_48 | |||||||||||||
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| 関連タイプ | isIdenticalTo | |||||||||||||
| 識別子タイプ | URI | |||||||||||||
| 関連識別子 | https://cir.nii.ac.jp/crid/1390282680057349248 | |||||||||||||
| 日本十進分類法 | ||||||||||||||
| 主題Scheme | NDC | |||||||||||||
| 主題 | 538 | |||||||||||||
| NCID | ||||||||||||||
| 収録物識別子タイプ | NCID | |||||||||||||
| 収録物識別子 | AA10925183 | |||||||||||||
| ISSN | ||||||||||||||
| 収録物識別子タイプ | EISSN | |||||||||||||
| 収録物識別子 | 2186-4772 | |||||||||||||
| ISSN | ||||||||||||||
| 収録物識別子タイプ | PISSN | |||||||||||||
| 収録物識別子 | 0911-551X | |||||||||||||
| 著作権関連情報 | ||||||||||||||
| 権利情報 | Copyright (c) 2012 Japanese Rocket Society | |||||||||||||
| キーワード | ||||||||||||||
| 主題Scheme | Other | |||||||||||||
| 主題 | space debris | |||||||||||||
| 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 | 7983 | |||||||||||||
