{"created":"2023-06-20T14:44:15.684939+00:00","id":11683,"links":{},"metadata":{"_buckets":{"deposit":"298fc954-9fa2-4c5e-9efc-06597adef72e"},"_deposit":{"created_by":1,"id":"11683","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"11683"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00011683","sets":["1543:1580:1596","1887:1891"]},"author_link":["103276","103277","103275","103274","103272","103273"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A study for a miniature helicopter to explore Mars"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"348","bibliographicPageStart":"345","bibliographic_titles":[{"bibliographic_title":"第3回宇宙科学シンポジウム"},{"bibliographic_title":"Proceedings of the 3rd Space Science Symposium","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Reported here is the study for the possibility and conceptual design of a miniature helicopter to explore Mars. If the helicopter is required only to take the pictures of targets and the form of the helicopter is so-called 'quad rotor' the total mass of the helicopter is estimated about 170 g. A simple experiment for the aerodynamic characteristic of a centimeter sized rotor in a vacuum chamber shows that it is not impossible for the helicopter to fly the Martian atmosphere.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045441078","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学 大学院工学系研究科"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"}]},"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":"都築, 範明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 俊逸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安部, 隆士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuzuki, Noriaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Shunichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Abe, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"MEMS","subitem_subject_scheme":"Other"},{"subitem_subject":"火星探査","subitem_subject_scheme":"Other"},{"subitem_subject":"微小ヘリコプタ","subitem_subject_scheme":"Other"},{"subitem_subject":"概念設計","subitem_subject_scheme":"Other"},{"subitem_subject":"ブレード負荷係数","subitem_subject_scheme":"Other"},{"subitem_subject":"クァドローター","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"低Reynolds数","subitem_subject_scheme":"Other"},{"subitem_subject":"CCDカメラ","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"MEMS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars exploration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"miniature helicopter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"conceptual design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blade load coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"quadrotor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low Reynolds number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CCD camera","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","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":"微小ヘリコプタ火星探査機に関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"微小ヘリコプタ火星探査機に関する研究"}]},"item_type_id":"5","owner":"1","path":["1596","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"11683","relation_version_is_last":true,"title":["微小ヘリコプタ火星探査機に関する研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T06:33:35.541752+00:00"}