{"created":"2023-06-20T15:09:07.645444+00:00","id":38631,"links":{},"metadata":{"_buckets":{"deposit":"ecce5cb2-d04f-4f47-9442-53a8bc07c77e"},"_deposit":{"created_by":1,"id":"38631","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38631"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038631","sets":["1887:1891"]},"author_link":["435122","435125","435126","435127","435120","435129","435123","435121","435124","435128"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-09","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{}]}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"15th European Space Mechanisms & Tribology Symposium - ESMATS 2013（September 25-27, 2013.), Noordwijk, The Netherlands.","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AC1400052000","subitem_description_type":"Other"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"European Space Agency(ESA)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"川崎重工業株式会社"},{"subitem_text_value":"川崎重工業株式会社"},{"subitem_text_value":"川崎重工業株式会社"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries LTD."},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries LTD."},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries LTD."}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"寺島, 啓太"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"紙田, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Horie, Youichi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Masakazu"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onikura, Hiroki"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Terashima, Keita","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kamita, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Horie, Youichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Masakazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onikura, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"DEVELOPMENT STATUS OF LOW-SHOCK PAYLOAD SEPARATION MECHANISM FOR H-IIA LAUNCH VEHICLE","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"DEVELOPMENT STATUS OF LOW-SHOCK PAYLOAD SEPARATION MECHANISM FOR H-IIA LAUNCH VEHICLE","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"38631","relation_version_is_last":true,"title":["DEVELOPMENT STATUS OF LOW-SHOCK PAYLOAD SEPARATION MECHANISM FOR H-IIA LAUNCH VEHICLE"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:38:10.218199+00:00"}