{"created":"2023-06-20T14:40:43.143455+00:00","id":7638,"links":{},"metadata":{"_buckets":{"deposit":"35e71afb-dc82-4803-9a7f-4fbe28bd408d"},"_deposit":{"created_by":1,"id":"7638","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7638"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007638","sets":["1543:1544:1559","1887:1891"]},"author_link":["40917","40915","40920","40918","40916","40921","40922","40919"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"クローバ型ソーラーセイルの膜面展開動力学"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"31","bibliographicPageStart":"25","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":"ISAS/JAXAでは、スピン型ソーラーセイルについて研究を行っている。本論文で扱うクローバ型セイルの展開は2段階に分けられる。この展開の解析モデルを確立するために、スピンテーブルおよびS-310観測ロケットを用い、それぞれ、直径2.5mと10mの膜面を動的に展開した。これらの運動は多粒子系モデルを用いた数値シミュレーション結果とよく一致した。一方、実機への応用を考えるとより大きな膜を準静的に展開する必要があり、大気球を用いた直径20mの膜面展開実験を予定している。本論文では、これらを実現するための展開機構についても紹介し、多粒子モデルによる数値シミュレーション結果を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"ISAS/JAXA is studying a deployment method using centrifugal force for solar sail mission. In this paper, the clover type sail is investigated. The deployment sequence consists of two stages. In order to establish the analytical model of sail deployment, two kinds of experiments using a spinning table and an S-310 sounding rocket are conducted. In these experiments, the clover type sails of 2.5 m and 10 m diameters are deployed dynamically. These motions coincide with the motions by the numerical simulations using multiparticle model. On the other hand, the larger sail is supposed to be deployed statically as for actual spacecraft. It is scheduled to deploy the sail of 20 m diameter using a high altitude balloon. The mechanisms for first and second stage deployments are introduced and the results of numerical simulation using multiparticle model are shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897005","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":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"東京大学 大学院"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"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 Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency 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":"森, 治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"津田, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西村, 祐介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mori, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishimura, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"展開","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"遠心力","subitem_subject_scheme":"Other"},{"subitem_subject":"観測ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"高高度気球","subitem_subject_scheme":"Other"},{"subitem_subject":"角速度","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"centrifugal force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sounding rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high altitude balloon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular velocity","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":"Deployment dynamics of clover type solar sail","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Deployment dynamics of clover type solar sail","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":"7638","relation_version_is_last":true,"title":["Deployment dynamics of clover type solar sail"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:23.682143+00:00"}