{"created":"2023-06-20T14:54:10.411125+00:00","id":22445,"links":{},"metadata":{"_buckets":{"deposit":"55f7720d-8516-40d9-8202-4e5437b0070e"},"_deposit":{"created_by":1,"id":"22445","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22445"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022445","sets":["1887:1888"]},"author_link":["210493","210487","210489","210485","210488","210492","210494","210486","210491","210490"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Ground Experiment for Development of Liquid Propellant Acquisition Devices under Microgravity"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"77","bibliographicPageStart":"73","bibliographicVolumeNumber":"12","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For future space transportation system development, efficient liquid propellant acquisition technologies under microgravity could berequired to realize long-term missions in orbit. Microgravity environment is generally established through drop tower, parabolic flight by airplane ororbital/suborbital experiment. These methods are large-scale or not flexible so that compact and simple method is needed for the efficientdevelopment. To respond to such request, we propose a static experiment on the ground to realize the similar static free surface under microgravity.The ground experimental result was compared with the results of two types of two-phase flow simulation codes for the verification of themethodology and discuss the characteristics of these numerical codes. We also simulated the free surface under the actual flight condition by usingthe same simulation method and result showed the validity of the experimental method.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1410086000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会(JSASS)"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences (JSASS)"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2322/astj.12.73"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2322/astj.12.73","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1884-0477","subitem_source_identifier_type":"ISSN"}]},"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":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"東京大学"}]},"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":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"The University of Tokyo"}]},"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":"杵淵, 紀世志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加納, 康仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"齊藤, 靖博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沖田, 耕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"姫野, 武洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kinefuchi, Kiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kano, Yasuhito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okita, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Himeno, Takehiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Liquid Rocket; Propellant Management; Surface Tension; Microgravity; Two-phase Flow","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":"微小重力下での液体推薬保持技術開発のための地上模擬実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"微小重力下での液体推薬保持技術開発のための地上模擬実験"}]},"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":"22445","relation_version_is_last":true,"title":["微小重力下での液体推薬保持技術開発のための地上模擬実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:21:02.259890+00:00"}