{"created":"2023-06-20T14:49:24.190483+00:00","id":17270,"links":{},"metadata":{"_buckets":{"deposit":"e939fba8-37ec-4fac-bfeb-3e166ed735ab"},"_deposit":{"created_by":1,"id":"17270","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"17270"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00017270","sets":["1543:1693:1709","1887:1891"]},"author_link":["156922","156923","156927","156926","156924","156928","156929","156925"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Reusable rocket demonstration vehicle system design"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"161","bibliographicPageStart":"158","bibliographic_titles":[{"bibliographic_title":"宇宙輸送シンポジウム　平成15年度"},{"bibliographic_title":"Proceedings of Space Transportation Symposium FY2003","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A baseline configuration of the reusable rocket demonstration vehicle is presented. The vehicle adopts a vertical take-off and vertical landing (VTVL) system to minimize ground support equipments (GSE) and turn-around time. The integrated propulsion system which consists of four LH2/LOX expander cycle engines, GH2/GOX reaction control system (RCS) and an assist power unit (APU). The vehicle is designed to meet the requirements of carrying 100 kg payload on a round trip to 120 km and repeating the mission within 24 hours.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047118040","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"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 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"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 Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"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":"小川, 博之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野中, 聡"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷口, 浩文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青木, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nonaka, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Taniguchi, Hirofumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoki, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ターンアラウンド","subitem_subject_scheme":"Other"},{"subitem_subject":"再使用ロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"垂直着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"垂直離陸","subitem_subject_scheme":"Other"},{"subitem_subject":"地上支援装置","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙輸送システム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_scheme":"Other"},{"subitem_subject":"turnaround","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reusable rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vertical landing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vertical takeoff","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground support equipment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space transportation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"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":"再使用観測ロケットのシステム検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再使用観測ロケットのシステム検討"}]},"item_type_id":"5","owner":"1","path":["1709","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"17270","relation_version_is_last":true,"title":["再使用観測ロケットのシステム検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:40:38.488048+00:00"}