{"created":"2023-06-20T14:48:37.425949+00:00","id":16448,"links":{},"metadata":{"_buckets":{"deposit":"6fb2e8e5-c50e-4f8c-af37-a3e078acfcbc"},"_deposit":{"created_by":1,"id":"16448","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16448"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016448","sets":["1543:1693:1702","1887:1891"]},"author_link":["149300","149297","149294","149295","149301","149303","149299","149302","149296","149298"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study on High-frequency Pulse Detonation Engine with a Rotary Valve"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"平成22年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium: FY2010","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22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 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 FY2010 (January 20-21, 2011. 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":"We proposed a novel rotary valve system for a pulse detonation rocket engine (PDRE). Since this valve can supply three gases (oxidizer, fuel, purge gas) into a pulse detonation tube (combustor) by using a single rotary disk, the total weight of this valve is very low. We carried out the optical and thrust measurements by using the PDRE system with the rotary valve and ethylene-oxygen propellant in order to confirm the thrust performance of the system. As a result, we confirmed the stable operation of the system over a wide range of operation frequency (40-160 Hz) and measured the time-averaged thrust. The maximum time-averaged thrust of 71.4 N and the maximum specific impulse of 232 sec were achieved at operation frequency of 160 Hz.","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: CD-ROM1枚","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":"Note: One CD-ROM","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065073001","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"}]},"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_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10324301","subitem_source_identifier_type":"NCID"}]},"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":"慶應義塾大学"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所"}]},"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":"Keio Univeristy"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"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":"笠原, 次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松岡, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"江角, 元貴"}],"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":"Matsuoka, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Esumi, Motoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuo, Akiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funaki, Ikko","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"Rotating Detonation Engine","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":"回転バルブを用いた高周波数作動 パルスデトネーションエンジンに関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"回転バルブを用いた高周波数作動 パルスデトネーションエンジンに関する研究"}]},"item_type_id":"5","owner":"1","path":["1702","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16448","relation_version_is_last":true,"title":["回転バルブを用いた高周波数作動 パルスデトネーションエンジンに関する研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:52:40.644876+00:00"}