{"created":"2023-06-20T14:48:24.116023+00:00","id":16203,"links":{},"metadata":{"_buckets":{"deposit":"89c83fa1-3a75-4eba-964f-d3baa20a49a7"},"_deposit":{"created_by":1,"id":"16203","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16203"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016203","sets":["1543:1693:1700","1887:1891"]},"author_link":["147043","147041","147044","147042","147045","147040"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study of Electric-motor Turbo Pump for Reusable Hybrid Rocket Engine"}]},"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":"A hybrid rocket engine is suitable for the reusable launch vehicle in low cost and safety. The authors study the hybrid rocket engine with a low cost fuel targeting the reusable launch vehicle like the Space Ship 2. For developing large-scale engines for the reusable launch vehicle, we conducted the hot firing tests of sub-scale hybrid rocket engines to obtain combustion characteristics of the low cost fuel. The fuel grains were multi-port type and wagon-wheel type, and the size of the grains was 160 mm in diameter and 350 mm in length, and the oxidizer was LOX. It was found that the ignition and combustion were very stable. We confirmed the burning time that more than 20-second duration was achieved.","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: AA0061856067","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-2012-067","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":"株式会社IHIエアロスペース"},{"subitem_text_value":"株式会社IHIエアロスペース"},{"subitem_text_value":"株式会社IHIエアロスペース"}]},"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":"IHI AEROSPACE Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"五十嵐, 真二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福地, 亜宝郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 研吾"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Igarashi, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukuchi, Aporo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Kengo","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":"61856067.pdf","filesize":[{"value":"371.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61856067.pdf","url":"https://jaxa.repo.nii.ac.jp/record/16203/files/61856067.pdf"},"version_id":"1a698871-7073-4c8a-a66c-88241da7b414"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Low cost fuel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reusable Hybrid Rocket 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":"低コスト燃料を用いたサブスケールハイブリッドロケットエンジンの燃焼特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低コスト燃料を用いたサブスケールハイブリッドロケットエンジンの燃焼特性"}]},"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":"16203","relation_version_is_last":true,"title":["低コスト燃料を用いたサブスケールハイブリッドロケットエンジンの燃焼特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:57:59.109610+00:00"}