{"created":"2023-06-20T15:09:07.512285+00:00","id":38629,"links":{},"metadata":{"_buckets":{"deposit":"79b03da1-1f88-4df1-a693-d9ff811a5441"},"_deposit":{"created_by":1,"id":"38629","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38629"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038629","sets":["1887:1891"]},"author_link":["435105","435101","435100","435099","435109","435102","435103","435108","435107","435098","435106","435104"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-07","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":"Joint Propulsion Conferences, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference（July 14-17, 2013.), San Jose, California, United States.","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Fundamental research activities have been conducted on LOX/Methane rocket engine to achieve higher performance for upper stage system of a middle class launch vehicle. The effects of combustion chamber pressure and mixture ratio on engine performance were demonstrated using a subscale engine test model in the High Altitude Test Stand. Highly expanded nozzle, area ratio of 71 was used in the HATS test to obtain thrust increment generated in the nozzle part. The combustion chamber pressure was changed as a parameter from 1 MPa to 3 MPa, mixture ratio was changed as a parameter from 2.8 to 3.6. Test results shows that specific impulse and thrust performance are increasing with combustion chamber pressure. On the other hand, effects of mixture ratio were small within the test condition.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AC1400050000","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: AIAA2013-4056","subitem_description_type":"Other"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"American Institute of Aeronautics and Astronautics(AIAA)"}]},"item_5_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2514/6.2013-4056"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2514/6.2013-4056","subitem_relation_type_select":"DOI"}}]},"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":"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":"株式会社IHIエアロスペース"},{"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":"Japan Aerospace Exploration Agency(JAXA)"},{"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":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"IHI AEROSPACE Co.,Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"}]},"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":"植田, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"冨田, 健夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野寺, 卓郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"久保田, 勲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kano, Yasuhito"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宗永, 隆男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomita, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onodera, Takuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kubota, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kano, Yasuhito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Munenaga, Takao","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":"Hot-Firing Test of Methane-Fueled Rocket Engine under High Altitude Condition","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Hot-Firing Test of Methane-Fueled Rocket Engine under High Altitude Condition","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":"38629","relation_version_is_last":true,"title":["Hot-Firing Test of Methane-Fueled Rocket Engine under High Altitude Condition"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:38:12.023180+00:00"}