{"created":"2023-06-20T14:49:24.055753+00:00","id":17268,"links":{},"metadata":{"_buckets":{"deposit":"544264c5-982c-42e1-bed4-d0edb28054fa"},"_deposit":{"created_by":1,"id":"17268","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"17268"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00017268","sets":["1543:1693:1709","1887:1891"]},"author_link":["156908","156914","156910","156916","156912","156913","156909","156917","156915","156911"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Conceptual design of a TBCC engine system for a space plane"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"153","bibliographicPageStart":"151","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"TSTOを2020年までに実現する計画がJAXAにて検討されている。その機体構成は、1段が空気吸込み式エンジン、2段が再使用ロケットエンジンの構成としたものである。一方、ATREXエンジンの改良を続け、エンジンによる基盤技術研究として、過去10年以上に渡り、能代多目的実験場にて試験データを蓄積してきた。ATREXエンジンのメリットとしては、高推力、簡易エンジン構造、低圧損なコアエンジン部などがあるが、一方デメリットとして低比推力および熱交換器用耐熱材の課題がある。特に、ATREXエンジンの高性能を引き出すためには、1,200K以上で作動可能な熱交換器として、加工性、耐熱性などの課題がクリア出来る材料の登場を待つ必要がある。これらの問題をカバーすべく、現状の技術で開発可能な、予冷ターボ式(PCTJ)エンジンを、TSTO用空気吸込み式エンジンの候補として選定検討した。その検討過程および試験計画などについて報告する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047118038","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":"アイ・エイチ・アイ・エアロスペース"},{"subitem_text_value":"アイ・エイチ・アイ・エアロスペース"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"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":"川井, 庸男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"太田, 豊彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 哲也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小林, 弘明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"棚次, 亘弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawai, Tsuneo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ota, Toyohiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Tetsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanatsugu, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"概念設計","subitem_subject_scheme":"Other"},{"subitem_subject":"再使用ロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"熱抵抗","subitem_subject_scheme":"Other"},{"subitem_subject":"タービンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"ATREXエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"空気取り込み","subitem_subject_scheme":"Other"},{"subitem_subject":"TSTO","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"conceptual design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reusable rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal resistance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbine engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ATREX engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air intake","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TSTO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","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":"スペースプレーン用TBCCエンジンのシステム概念設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スペースプレーン用TBCCエンジンのシステム概念設計"}]},"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":"17268","relation_version_is_last":true,"title":["スペースプレーン用TBCCエンジンのシステム概念設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:40:40.143098+00:00"}