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DEVELOPMENT STATUS OF LOW-SHOCK PAYLOAD SEPARATION MECHANISM FOR H-IIA LAUNCH VEHICLE
https://jaxa.repo.nii.ac.jp/records/38631
https://jaxa.repo.nii.ac.jp/records/3863173c8e593-fa89-4546-9a86-5b8540628cdd
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | DEVELOPMENT STATUS OF LOW-SHOCK PAYLOAD SEPARATION MECHANISM FOR H-IIA LAUNCH VEHICLE | |||||
言語 | ||||||
言語 | eng | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
寺島, 啓太
× 寺島, 啓太× 紙田, 徹× Horie, Youichi× Kobayashi, Masakazu× Onikura, Hiroki× Terashima, Keita× Kamita, Toru× Horie, Youichi× Kobayashi, Masakazu× Onikura, Hiroki |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
川崎重工業株式会社 | ||||||
著者所属 | ||||||
川崎重工業株式会社 | ||||||
著者所属 | ||||||
川崎重工業株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries LTD. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries LTD. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries LTD. | ||||||
出版者(英) | ||||||
出版者 | European Space Agency(ESA) | |||||
書誌情報 | 発行日 2013-09 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 15th European Space Mechanisms & Tribology Symposium - ESMATS 2013(September 25-27, 2013.), Noordwijk, The Netherlands. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents the design, analysis and test results of the low-shock payload separation mechanism for the H-IIA launch vehicle. The mechanism is based on a simple and reliable four-bar linkage, which makes the release speed of the marman clamp band tension lower than the current system.The adequacy of the principle for low-shock mechanism was evaluated by some simulations and results of fundamental tests. Then, we established the reliabilitydesign model of this mechanism, and the adequacy of this model was evaluated by elemental tests. Finally, we conducted the system separation tests usingthe payload adapter to which the mechanism was assembled, to confirm that the actual separation shock level satisfied our target. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1400052000 |