{"created":"2023-06-20T14:54:14.067627+00:00","id":22524,"links":{},"metadata":{"_buckets":{"deposit":"40098d26-7397-4301-a92d-9bf6dd83fa8b"},"_deposit":{"created_by":1,"id":"22524","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22524"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022524","sets":["1887:1888"]},"author_link":["211147","211143","211146","211148","211145","211144","211142"],"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-07","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{}]}]},"item_7_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":"50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference（July 28-30, 2014.), Cleveland, OH, United States.","subitem_description_type":"Other"}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Helium solubility in propellant causes pressure drop in tank for bipropellant system.\nThere is a restriction that tank pressure is controlled in narrow range limited by maximum\ndesign pressure of a component and minimum thrust to control attitude. Tank pressure\ndecreases with helium solubility for some tens day after tank pressurization on the ground.\nIt is necessary to predict the pressure drop. Analytical solubility model has been developed\nas prediction method of the pressure drop. The prediction corresponds to the data of Apollo\nand some satellites. However, the conventional model was assumed that the tank was static.\nIn H-II Transfer Vehicle (HTV), propellant sloshing occurred by movement of HTV between\nbuildings on the ground. Tank pressure drop of HTV could not be predicted by the\nconventional model because of the sloshing. This research presents numerical solubility\nmodel which expresses the influence of sloshing on helium solubility with solving distribution\nof helium concentration.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1510022000","subitem_description_type":"Other"}]},"item_7_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: AIAA 2014-3567","subitem_description_type":"Other"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"American Institute of Aeronautics and Astronautics (AIAA)"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2514/6.2014-3567"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2514/6.2014-3567","subitem_relation_type_select":"DOI"}}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industry"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industry"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industry"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industry"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industry"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"}]},"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":"Kurishita, Yuto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noritake, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuyama, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masuda, Kazumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyanaga, Masafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Himeno, Takehiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takata, Shinichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"HTV Numerical Simulation Model of the Helium Solubility in the Propellant","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HTV Numerical Simulation Model of the Helium Solubility in the Propellant","subitem_title_language":"en"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-06-02"},"publish_date":"2015-06-02","publish_status":"0","recid":"22524","relation_version_is_last":true,"title":["HTV Numerical Simulation Model of the Helium Solubility in the Propellant"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:19:43.643754+00:00"}