{"created":"2023-06-20T15:11:31.793099+00:00","id":41209,"links":{},"metadata":{"_buckets":{"deposit":"173a77c7-2136-4501-ba52-8e795e41ffaf"},"_deposit":{"created_by":1,"id":"41209","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41209"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041209","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451180","451178","451182","451183","451179","451181"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Combustion characteristics of metallized hydrocarbon fuels"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"14","bibliographicPageStart":"1","bibliographicVolumeNumber":"1224","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"LOX(液体酸素)/炭化水素に金属を添加した3推進薬の燃焼特性の評価を行った。比推力、密度比推力および燃焼特性を評価するため、LOX/ケロシン/Be,LOX/ケロシン/B,LOX/ケロシン/Mg,LOX/ケロシン/Alの3推進薬について熱化学性能計算を行った。LOX/ケロシン/Beの比推力が2推進薬に優る事を示し、Al、Mg、Bのような高密度要素を利用する密度比推力の考え方を立証した。単段インジェクタ、水冷燃焼室を用いて酸素/ケロシン/Alの3推進薬の燃焼特性評価試験を行った。相違する2種類の噴流衝突型インジェクタ(F-O-F)を液体酸素用に、また同軸インジェクタを気体酸素用に用いた。供試燃料はケロシンに1.9-3.1μm粒径のアルミニウム粉体を懸濁させたものを用いた。アルミニウムの濃度は1-20重量％で変化させた。試験燃焼圧は4MPa,混合比は1.4-5.1であった。ケロシンにアルミニウムを添加したこれらの試験の結果、噴流衝突型インジェクタでは燃焼安定性が大幅に改善され、また同軸インジェクタではC｛*｝効率の増強が達成された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper the combustion performance of tripropellants consisting of LOX (Liquid OXygen)/hydrocarbon fuel and solid metals was evaluated. Thermochemical calculations were performed to evaluate specific impulse, specific density impulse and the combustion properties of LOX/kerosene/Be, LOX/kerosene/B, LOX/kerosene/Mg and LOX/kerosene/Al tripropellants. The specific impulse advantage of LOX/kerosene/Be over bipropelfants was demonstrated. Experiments were conducted to evaluate the combustion characteristics of oxygen and kerosene/aluminum tripropellants using single-element injectors and a water-cooled combustion chamber. Two kinds of unlike impinging element (F-O-F (Fuel-Oxygen-Fuel)) injectors were tested using liquid oxygen and one kind of coaxjul injector  was tested using gaseous oxygen. The fuel used was a kerosene and aluminum mixture which consisted of aluminum particles, with a meam diameter of 1.9 to 3.1 micrometer in mean diameter, suspended in kerosene fuel.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004239000","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: NAL TR-1224","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 ロケット推進研究部"},{"subitem_text_value":"航空宇宙技術研究所 ラムジェット推進研究部"},{"subitem_text_value":"航空宇宙技術研究所 ラムジェット推進研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Rocket Propulsion Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"坂本, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 和雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"八柳, 信之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakamoto, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yatsuyanagi, Nobuyuki","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01224.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01224.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41209/files/naltr01224.pdf"},"version_id":"289496e7-bc56-48b7-94fe-67f78e10c763"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"3推進薬","subitem_subject_scheme":"Other"},{"subitem_subject":"金属添加燃料","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"液体酸素","subitem_subject_scheme":"Other"},{"subitem_subject":"炭化水素","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼特性","subitem_subject_scheme":"Other"},{"subitem_subject":"比推力","subitem_subject_scheme":"Other"},{"subitem_subject":"密度比推力","subitem_subject_scheme":"Other"},{"subitem_subject":"ケロシン","subitem_subject_scheme":"Other"},{"subitem_subject":"ほう素","subitem_subject_scheme":"Other"},{"subitem_subject":"ベリリウム","subitem_subject_scheme":"Other"},{"subitem_subject":"マグネシウム","subitem_subject_scheme":"Other"},{"subitem_subject":"アルミニウム","subitem_subject_scheme":"Other"},{"subitem_subject":"性能計算","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼試験","subitem_subject_scheme":"Other"},{"subitem_subject":"tripropellant","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"metallized fuel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"liquid oxygen","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hydrocarbon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"specific thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"specific density thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"kerosene","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boron","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"beryllium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnesium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aluminum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion test","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"金属添加炭化水素ロケットの燃焼特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"金属添加炭化水素ロケットの燃焼特性"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41209","relation_version_is_last":true,"title":["金属添加炭化水素ロケットの燃焼特性"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:04.255289+00:00"}