{"created":"2023-06-20T15:09:05.421405+00:00","id":38597,"links":{},"metadata":{"_buckets":{"deposit":"6ca6fcb5-2577-40fb-b4f1-0f83ba0304b3"},"_deposit":{"created_by":1,"id":"38597","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38597"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038597","sets":["1887:1891"]},"author_link":["434803","434805","434807","434804","434806","434802"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-10","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"第57回宇宙科学技術連合講演会講演集"},{"bibliographic_title":"Proceedings of 57th Space Sciences and Technology Conference","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The component of a satellite falling to the ground is a crucial problem，since titanium tanks are one of the components causing most damage to the ground in satellites. To replace titanium tanks，JAXA has researched a Melting Promotion Type Tank  which can reduce  residual debris during the  re-entry  phase，The tank structure  freatures an alurninum liner overwrapped with carbon composite (filament winding).The basic design，traial manufacture，scale model PMD (propellant  Management Device) test under low gravity，CFRP  out gassing property acquisition and CFRP resistance to radiation tests were conducted in a  research phase. This paper also describes the development plan of this tank.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AC1400013000","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JSASS-2013-4602","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences"}]},"item_5_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":"株式会社IHIエアロスペース"}]},"item_5_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":"IHI　Aerospace"}]},"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":"升岡, 正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"増田, 井出夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masuoka, Tadashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masuda, Ideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Tank; Propellant; Hydrazine; Re-entry; Propulsion system","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"衛星用再突入時溶融促進型推進薬タンクの研究開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"衛星用再突入時溶融促進型推進薬タンクの研究開発"}]},"item_type_id":"5","owner":"1","path":["1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"38597","relation_version_is_last":true,"title":["衛星用再突入時溶融促進型推進薬タンクの研究開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:38:43.949761+00:00"}