{"created":"2023-06-20T14:35:59.825962+00:00","id":2290,"links":{},"metadata":{"_buckets":{"deposit":"ad381741-0ac8-4ae9-a460-873f71f199f0"},"_deposit":{"created_by":1,"id":"2290","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2290"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002290","sets":["1398:1408:1418","1887:1893","9:10:256:297"]},"author_link":["5020","5017","5013","5010","5008","5012","5011","5019","5018","5021","5016","5009","5014","5015"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Static deployment experiment of solar sail membrane using a balloon"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-01-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"56","bibliographicPageStart":"31","bibliographicVolumeNumber":"JAXA-RR-05-012","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告: 大気球研究報告"},{"bibliographic_title":"JAXA Research and Development Report: Research Reports on High Altitude Balloons","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ISAS/JAXAが提案しているソーラー電力セイルでは直径50m程度の膜面を準静的に展開する必要がある。この膜面展開機構を提案し、大気球実験により実証することとした。本論文では、このための準備としてスピンテーブルを用いてクローバ型の展開実験を行い、1次展開と2次展開を連続して行うための膜面の折り方や形状を検討する。次に、多粒子系モデルを用いた数値シミュレーションによって展開運動を解析し、気球実験のための膜面のサイジングや準静的展開機構を用いた運動の検証を行う。さらに、これを踏まえて構築した実験システムを紹介し、最後に、得られた実験結果について詳細に考察する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"One of the most important assignments of the solar powered sail proposed in ISAS/JAXA is the static deployment of its membrane whose diameter is about 50 m. The demonstration of the deployment mechanism is performed using a balloon. First, the sail shape and its folding pattern are investigated by the dynamic deployment using a spinning table. Next, the deployment motion is analyzed by numerical simulations using multi-particle model in order to decide the sail size. Finally, the experiment system is introduced and the experiment results are shown in detail.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049046003","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RR-05-012","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_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":"東京大学 大学院工学系研究科"},{"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 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":"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"}]},"item_3_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":"University of Tokyo School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo School of Engineering"},{"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":"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"森, 治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中納, 知樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"多羅尾, 康太"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"志田, 真樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"津田, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐伯, 高尚"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mori, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakano, Tomoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tarao, Kota","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shida, Maki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saiki, Takanao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"49046003.pdf","filesize":[{"value":"7.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49046003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2290/files/49046003.pdf"},"version_id":"d8ae4263-7dab-46f4-b5ac-b6ebaaa1138a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"ポリエチレンテレフタレート","subitem_subject_scheme":"Other"},{"subitem_subject":"準静的展開","subitem_subject_scheme":"Other"},{"subitem_subject":"展開運動","subitem_subject_scheme":"Other"},{"subitem_subject":"展開メカニズム","subitem_subject_scheme":"Other"},{"subitem_subject":"多粒子モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"デジタルシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"動きのシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽センサ","subitem_subject_scheme":"Other"},{"subitem_subject":"気球","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"polyethylene terephthalate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"quasi-static deployment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"deployment mechanism","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multi-particle model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"digital simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motion simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balloon","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"大気球を用いたソーラーセイル膜面の準静的展開実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"大気球を用いたソーラーセイル膜面の準静的展開実験"}]},"item_type_id":"3","owner":"1","path":["297","1418","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2290","relation_version_is_last":true,"title":["大気球を用いたソーラーセイル膜面の準静的展開実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:25:12.943802+00:00"}