{"created":"2023-06-20T14:54:08.088034+00:00","id":22394,"links":{},"metadata":{"_buckets":{"deposit":"cbb5ea2a-cd71-4fd7-a38f-eaa7545f205a"},"_deposit":{"created_by":1,"id":"22394","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22394"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022394","sets":["1887:1888"]},"author_link":["209924","209922","209921","209923"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Heat Transfer Characteristics with Boiling of the Propellant(N2O4) for Spacecraft Propulsion"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-01","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4","bibliographicPageEnd":"433","bibliographicPageStart":"427","bibliographicVolumeNumber":"27","bibliographic_titles":[{"bibliographic_title":"混相流"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"MON3 is used as a propellant for the bipropellant thruster in the spacecraft propulsion. MON3 is Nitrogen Tetroxide (N2H4) with 3wt% solution of NO. Heat transfer characteristics with boiling of the MON3 have been measured. The critical heat transfer was identified when the superheat temperature was around 50 ℃ (degree C) under different flow parameters. Pressure vibration from 8 to 22Hz frequency was observed in the specific flow parameters during the boiling of MON3. These frequencies are in good agreement with that of combustion perturbations observed in the test injector which simulated the actual bipropellant thrusters.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1410027000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本混相流学会"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"THE JAPANESE SOCIETY FOR MULTIPHASE FLOW"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.3811/jjmf.27.427"}],"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.3811/jjmf.27.427","subitem_relation_type_select":"DOI"}}]},"item_7_rights_28":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"(C)2013 日本混相流学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0914-2843","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10088286","subitem_source_identifier_type":"NCID"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"株式会社　IHIエアロスペース"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"IHI AEROSPACE Co.,Ltd."}]},"item_7_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"長田, 泰一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松浦, 芳樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagata, Taiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuura, Yoshiki","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":"2020-01-22"}],"displaytype":"detail","filename":"PA1410027.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"PA1410027.pdf","url":"https://jaxa.repo.nii.ac.jp/record/22394/files/PA1410027.pdf"},"version_id":"6cb6d521-530a-4502-ae3b-7696e528debd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Heat transfer with boiling; Critical heat transfer; Nitrogen Tetroxide; Bipropellant thruster; Spacecraft propulsion","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"人工衛星推進系における推進薬（四酸化二窒素）の沸騰伝熱特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"人工衛星推進系における推進薬（四酸化二窒素）の沸騰伝熱特性"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"22394","relation_version_is_last":true,"title":["人工衛星推進系における推進薬（四酸化二窒素）の沸騰伝熱特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:21:55.180350+00:00"}