{"created":"2023-06-20T14:54:16.689980+00:00","id":22583,"links":{},"metadata":{"_buckets":{"deposit":"78454482-f801-4869-8182-791911fff056"},"_deposit":{"created_by":1,"id":"22583","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22583"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022583","sets":["1887:1888"]},"author_link":["211512","211513","211510","211511"],"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-11","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2","bibliographicPageEnd":"544","bibliographicPageStart":"538","bibliographicVolumeNumber":"104","bibliographic_titles":[{},{"bibliographic_title":"Acta Astronautica","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"JAXA has commenced technical research for contributing as a part of international partnership for the space exploration in Lunar vicinity. One of the candidates is the cargo transport mission with the combination of Cryogenic Propulsion Stage(s) (CPS) and a transfer vehicle derived from Japanese un-manned vehicle used for ISS. The CPS needs advanced technologies to keep the propellant for long mission duration and they will be useful in further missions beyond moon. This paper reports the profile of the mission, vehicle configurations, and the transport capabilities.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1510091000","subitem_description_type":"Other"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Elsevier"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.1016/j.actaastro.2014.06.014"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.1016/j.actaastro.2014.06.014","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0094-5765","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":"AA0050648X","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次世代宇宙船研究開発室(JAXA): 宇宙航空研究開発機構月・惑星探査プログラムグループ(JAXA)(JSPEC)"},{"subitem_text_value":"宇宙航空研究開発機構月・惑星探査プログラムグループ(JAXA)(JSPEC)"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Next Generation Space Vehicle Office, Japan Aerospace Exploration Agency (JAXA): JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA) (JSPEC)"},{"subitem_text_language":"en","subitem_text_value":"JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)"}]},"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":"今田, 高峰"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Imada, Takane","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"EML-2","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Lunar","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"OTV","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Rendezvous","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Cryogenic propulsion stage","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"Study on JAXA elements for international lunar vicinity mission","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Study on JAXA elements for international lunar vicinity mission","subitem_title_language":"en"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-09-14"},"publish_date":"2015-09-14","publish_status":"0","recid":"22583","relation_version_is_last":true,"title":["Study on JAXA elements for international lunar vicinity mission"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:18:42.340534+00:00"}