{"created":"2023-06-20T15:14:52.697205+00:00","id":44890,"links":{},"metadata":{"_buckets":{"deposit":"7a8028b5-5730-42ba-b12b-c39564a1e091"},"_deposit":{"created_by":1,"id":"44890","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44890"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044890","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["471770","471771","471769","471772"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"高性能推進薬の研究-酵素・リチウム・水素プロペラント-"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1980-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"26","bibliographicVolumeNumber":"635","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-635","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The performance potential of the 02/Li/H2 tripropellant combination is among the highest available from chemical propellants. Theoretical performance calculations were made for L-02/L-Li in the mixture ratio range of 0.6 to 3.0 at the chamber pressure of 5 to 50 atm, with liquid hydrogen addition ranging from 0 to 35 percent of the total propellant flowrate. Results of the computations are presented in a series of curves, which show the variations in an important performance parameter (Isp, cf, C, etc) including proportions of hydrogen, mixture ratio, chamber pressure, and nozzle expansion area ratios. An experimental was performed to investigate the feasibility of the 02/Li/H2 tripropellant combination. The experimental firing results are presented in curves, which show the variations of characteristic exhaust velocity efficiencies taking into consideration the factors, such as lithium weight ratios, chamber length, lithium injection angles, and gas generator mixture ratios. Uncorrected characteristic velocity efficiencies were 80 to 88 percent, showing that the use of this tripropellant combination is feasible.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0635000","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-635","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角田支所"},{"subitem_text_value":"航空宇宙技術研究所角田支所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"毛呂, 明夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 和雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORO, Akio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SUZUKI, Kazuo","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00635.pdf","filesize":[{"value":"3.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00635.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44890/files/naltr00635.pdf"},"version_id":"40ce2ded-0eab-485c-baba-63dc0fb62057"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"High Performance Propellant Study-Oxygen Lithium Hydrogen Tripropellant-","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"High Performance Propellant Study-Oxygen Lithium Hydrogen Tripropellant-","subitem_title_language":"en"}]},"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":"44890","relation_version_is_last":true,"title":["High Performance Propellant Study-Oxygen Lithium Hydrogen Tripropellant-"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:49:02.359399+00:00"}