{"created":"2023-06-20T14:35:49.580997+00:00","id":2104,"links":{},"metadata":{"_buckets":{"deposit":"3c062b00-4590-4009-8f9d-a6ee127e1f69"},"_deposit":{"created_by":1,"id":"2104","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2104"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002104","sets":["1887:1893","9:10:132:133"]},"author_link":["3263","3256","3257","3265","3264","3272","3258","3259","3267","3261","3255","3269","3254","3274","3275","3268","3277","3266","3252","3276","3271","3273","3270","3253","3260","3262"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of a hypersonic turbojet engine controller designed for a flight experiment"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03-31","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-08-012","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXAでは，マッハ5クラスの極超音速機へ搭載するための極超音速ターボジェットエンジンの開発研究を進めている．このエンジンの特徴は，液体水素燃料の冷熱を利用して圧縮機入口の空気を冷却する空気予冷却サイクルを採用している点にあり，これによって従来のターボジェットエンジンでは動作不可能な極超音速飛行が可能になる．現在，推力100kgf級のサブスケールエンジンを製作し，飛行実験機搭載形態での地上燃焼試験を実施している．本稿では，極超音速ターボジェットエンジンの飛行実験用に開発した搭載型エンジン制御装置の設計と，地上実験による性能確認結果を示す．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The pre-cooled turbojet engine is one of the most promising candidates for the propulsion system of hypersonic transport. A notable feature of this engine is to use an air pre-cooling device using liquid hydrogen fuel as a coolant in order to protect the turbo-machinery from aerodynamic heating under hypersonic flight conditions. JAXA's recent model of the pre-cooled turbojet engine called \"S-Engine\" has 0.225 by 0.225 meters square cross section, a total length of 2.67 m, and a mass of 134 kg. It produces a thrust of 122 kgf by firing liquid hydrogen fuel in afterburner, its compressor rotational speed is 80,000 rpm and its compressor pressure ratio is six. This engine is developed for the flight test at Mach 2 condition integrated with a balloon-launched missile-like vehicle. This paper describes pre-flight verification test results of the engine control system including liquid hydrogen supplying system.","subitem_description_type":"Other"}]},"item_3_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"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064349000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RR-08-012","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙航行システム研究系"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部未踏技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム"},{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ無人機・未来型航空機チーム"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部宇宙航行システム研究系"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部ジェットエンジン技術研究センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Systems and Astronautics, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Unmanned and Innovative Aircraft Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Systems and Astronautics, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小林, 弘明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田口, 秀之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"澤井, 秀次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 和央"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小島, 孝之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岡井, 敬一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"本郷, 素行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"正木, 大作"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石塚, 只夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"原田, 賢哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"丸, 祐介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二村, 尚夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳, 良二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Taguchi, Hideyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawai, Shujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Kazuhisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kojima, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okai, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hongo, Motoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masaki, Daisaku","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishizuka, Tadao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Harada, Kenya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maru, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Futamura, Hisao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagi, Ryoji","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":"2020-01-15"}],"displaytype":"detail","filename":"64349000.pdf","filesize":[{"value":"8.3 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report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"飛行実験用極超音速ターボジェットエンジン制御装置の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"飛行実験用極超音速ターボジェットエンジン制御装置の開発"}]},"item_type_id":"3","owner":"1","path":["133","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2104","relation_version_is_last":true,"title":["飛行実験用極超音速ターボジェットエンジン制御装置の開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:28:34.710978+00:00"}