{"created":"2023-06-20T14:48:23.882172+00:00","id":16198,"links":{},"metadata":{"_buckets":{"deposit":"44a26ecc-6bea-4e40-a52d-9366ff6bbcde"},"_deposit":{"created_by":1,"id":"16198","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16198"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016198","sets":["1543:1693:1700","1887:1891"]},"author_link":["147019","147007","147015","147016","147005","147010","147009","147004","147006","147008","147017","147018","147012","147014","147013","147011"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research and Development of a Rotary-valved Four-cylinder Pulse Detonation Engine flight Test Model"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-01","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"平成24年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium: FY2012","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県","subitem_description_type":"Other"}]},"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":"Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Thrust-measurement experiment was carried out using a four-cylinder pulse detonation rocket engine (PDRE) with a rotary valve. This PDRE used three types of gases, oxidizer (N2O), fuel (C2H4), and purge gas (He) to generate detonation wave intermittently. We used a rotary valve attached coaxially to a motor for supplying these three gases. We achieved time-averaged thrust of 258.5 N and specific impulse of 138.7 sec in the operation for 1000 msec.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"},{"subitem_description":"形態: PDF","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"},{"subitem_description":"Physical characteristics: PDF","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0061856062","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: STCP-2012-062","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所(JAXA)(ISAS)"}]},"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":"筑波大学"},{"subitem_text_value":"筑波大学"},{"subitem_text_value":"筑波大学"},{"subitem_text_value":"筑波大学"},{"subitem_text_value":"筑波大学"},{"subitem_text_value":"広島大学"},{"subitem_text_value":"慶應義塾大学"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tsukuba"},{"subitem_text_language":"en","subitem_text_value":"University of Tsukuba"},{"subitem_text_language":"en","subitem_text_value":"University of Tsukuba"},{"subitem_text_language":"en","subitem_text_value":"University of Tsukuba"},{"subitem_text_language":"en","subitem_text_value":"University of Tsukuba"},{"subitem_text_language":"en","subitem_text_value":"Hiroshima University"},{"subitem_text_language":"en","subitem_text_value":"Keio University"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"笠原, 次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂本, 龍基"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"両角, 智人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柏崎, 貴司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤原, 大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松岡, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松尾, 亜紀子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"船木, 一幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kasahara, Jiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakamoto, Ryuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Morozumi, Tomohito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kashiwazaki, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujiwara, Yutaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuoka, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuo, Akiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funaki, Ikko","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-20"}],"displaytype":"detail","filename":"61856062.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61856062.pdf","url":"https://jaxa.repo.nii.ac.jp/record/16198/files/61856062.pdf"},"version_id":"52d81f8b-ebfc-4439-a9c7-d660ec098361"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Detonation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pulse Detonation Engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flight Test","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":"回転バルブ式４気筒パルスデトネーションエンジン飛行試験機の研究開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"回転バルブ式４気筒パルスデトネーションエンジン飛行試験機の研究開発"}]},"item_type_id":"5","owner":"1","path":["1700","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16198","relation_version_is_last":true,"title":["回転バルブ式４気筒パルスデトネーションエンジン飛行試験機の研究開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:58:08.946085+00:00"}