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Development of Equipment to Estimate Momentum Shift in NEO Orbit Change by a Spacecraft Impact
http://hdl.handle.net/10228/00007234
http://hdl.handle.net/10228/000072344fd3331a-088d-4497-9897-c55a1c3337b4
名前 / ファイル | ライセンス | アクション |
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LaSEINE-2015_17.pdf (1.1 MB)
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Item type | 会議発表論文 = Conference Paper(1) | |||||||||||
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公開日 | 2019-06-20 | |||||||||||
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 Equipment to Estimate Momentum Shift in NEO Orbit Change by a Spacecraft Impact | |||||||||||
言語 | ||||||||||||
言語 | eng | |||||||||||
著者 |
Kage, Shohei
× Kage, Shohei× Uenishi, Satoshi× Tanaka, Masashi× Koura, Takao× 赤星, 保浩
WEKO
5459
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抄録 | ||||||||||||
内容記述タイプ | Abstract | |||||||||||
内容記述 | For assessing the NEO orbit change by spacecraft impact, it is necessary to clarify the momentum shift at the impact time. Momentum shift is various amounts depending on the material of projectile and target, their shapes, and impact velocity. Currently, we have to collect more impact data by performing a simulated impact test on the earth because we do not have enough data to discuss design of a spacecraft impacter. Generally speaking, momentum shift is described at β (= about 1 ∼ 10 in other institution's impact tests). We aim to get more efficient momentum shift by creating experimental conditions in which β is larger than 10. In this study, we developed a test equipment of pendulum type for measuring β, and performed impact tests after calibration of the pendulum equipment. | |||||||||||
備考 | ||||||||||||
内容記述タイプ | Other | |||||||||||
内容記述 | 2015 Hypervelocity Impact Symposium (HVIS 2015), April 27-30, 2015, Boulder, Colorado | |||||||||||
書誌情報 |
Procedia Engineering 巻 103, p. 273-278, 発行日 2015-04 |
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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.2015.04.047 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | ISSN | |||||||||||
収録物識別子 | 1877-7058 | |||||||||||
著作権関連情報 | ||||||||||||
権利情報 | Copyright (c) 2015 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/). | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | Hypervelocity impact | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | momentum shift | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | space guard | |||||||||||
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 | ||||||||||||
7704 | ||||||||||||
著者所属 | ||||||||||||
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan | ||||||||||||
著者所属 | ||||||||||||
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan | ||||||||||||
著者所属 | ||||||||||||
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan | ||||||||||||
著者所属 | ||||||||||||
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan | ||||||||||||
著者所属 | ||||||||||||
Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1 – 1 Sensui, Tobata, Kitakyushu, Fukuoka 804-8550, Japan | ||||||||||||
資料タイプ | ||||||||||||
内容記述タイプ | Other | |||||||||||
内容記述 | Conference Paper |