{"created":"2023-06-20T14:40:43.945731+00:00","id":7656,"links":{},"metadata":{"_buckets":{"deposit":"151e5b7a-bca1-493b-875e-6164e1e9997a"},"_deposit":{"created_by":1,"id":"7656","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7656"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007656","sets":["1543:1544:1559","1887:1891"]},"author_link":["41025","41021","41026","41024","41022","41023"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"火星探査のためのロータクラフト機の検討"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"133","bibliographicPageStart":"127","bibliographic_titles":[{"bibliographic_title":"平成16年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"火星地表探査においてローバと組になって探査を行うロータークラフト機の可能性についての検討を行う。このようなロータークラフト機の併用により、ローバの活動性を向上させることが可能である。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An aerial vehicle operating under the command of a rover has a potential to extend the coverage for Mars exploration. Especially, a rotorcraft equipped with an imaging camera can gather geographic information around the rover and enables making of a smart strategy for the exploration. The development of such a rotorcraft, however, must solve some difficulty due to the thin Mars atmosphere. This is because the aerodynamic characteristics of the rotor depend mainly on the Reynolds number (Re) that decreases due to the thin atmosphere. In this paper, the aerodynamic characteristics of rotors were experimentally investigated to access a capability of the hover performance of the rotor in a very low Reynolds number regime (Re = 10(exp 3) to 10(exp 4), Ultra-low Reynolds number) that is expected in the thin Mars atmosphere. Based on the experimental investigation, the feasibility of such a rotorcraft was demonstrated.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897023","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"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":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"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":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"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":"予備調査","subitem_subject_scheme":"Other"},{"subitem_subject":"実験研究","subitem_subject_scheme":"Other"},{"subitem_subject":"回転翼航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"火星探査","subitem_subject_scheme":"Other"},{"subitem_subject":"ロービング機","subitem_subject_scheme":"Other"},{"subitem_subject":"火星大気","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行条件","subitem_subject_scheme":"Other"},{"subitem_subject":"feasibility study","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experimental investigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotary wing aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars exploration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"roving vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars atmosphere","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight condition","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Feasibility study for a small Mars exploration rotorcraft","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Feasibility study for a small Mars exploration rotorcraft","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7656","relation_version_is_last":true,"title":["Feasibility study for a small Mars exploration rotorcraft"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:06.914188+00:00"}