{"created":"2023-06-20T14:40:40.344030+00:00","id":7589,"links":{},"metadata":{"_buckets":{"deposit":"8c3c1da9-78f8-481f-883f-ba7a713f615e"},"_deposit":{"created_by":1,"id":"7589","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7589"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007589","sets":["1543:1544:1558","1887:1891"]},"author_link":["40631","40630","40632","40633"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"2重波折りパターンをなす2次元展開ソーラーセイル膜面のスピン展開制御実験"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"152","bibliographicPageStart":"147","bibliographic_titles":[{"bibliographic_title":"第15回アストロダイナミクスシンポジウム講演後刷り集　2005"},{"bibliographic_title":"Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"スピン展開型ソーラーセイル膜面の折り畳みとして提案する「2重波折りパターン」の展開動特性を実験的に明らかにするとともに、テザーで制御された展開を行うための展開機構の検討ならびに試作・展開制御実験を行い、展開制御特性について検討する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Deployment characteristics of spinning membrane are significant to realize the solar sail missions. This paper describes results and discussions about deployment experiments focused on dynamic properties of deployable spinning membranes for solar sail. In this study, we used the rotationally skew fold membrane models, and consider the effects of radius, folding pitch and membrane thickness. The results indicate that the membrane with smaller folding pitch is deployed quickly and larger radius causes rapidly deployment at the first stage of deployment. The wrapping direction which is equal to the spinning direction indicates the quickly deployment. Finally, the deployment characteristics of uncontrolled and controlled deployment of the rotationally skew fold membrane are discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063480024","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_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京工業大学"},{"subitem_text_value":"東京工業大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology"}]},"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":"古谷, 寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"井上, 陽介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Furuya, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inoue, Yosuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"折畳み構造","subitem_subject_scheme":"Other"},{"subitem_subject":"膜","subitem_subject_scheme":"Other"},{"subitem_subject":"展開","subitem_subject_scheme":"Other"},{"subitem_subject":"動特性","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"実験","subitem_subject_scheme":"Other"},{"subitem_subject":"ポリイミド","subitem_subject_scheme":"Other"},{"subitem_subject":"展開プロセス","subitem_subject_scheme":"Other"},{"subitem_subject":"展開率","subitem_subject_scheme":"Other"},{"subitem_subject":"folding structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"membrane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experimentation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"polyimide","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment ratio","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":"Tether controlled deployment characteristics of rotationally skew fold membrane for spinning solar sail","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Tether controlled deployment characteristics of rotationally skew fold membrane for spinning solar sail","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1558","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7589","relation_version_is_last":true,"title":["Tether controlled deployment characteristics of rotationally skew fold membrane for spinning solar sail"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:37:10.043993+00:00"}