{"created":"2023-06-20T14:46:49.917480+00:00","id":14431,"links":{},"metadata":{"_buckets":{"deposit":"89c860b3-feaf-4ea9-a9b9-d03b307c6da6"},"_deposit":{"created_by":1,"id":"14431","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14431"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014431","sets":["1543:1656:1664","1887:1891"]},"author_link":["132116","132124","132121","132117","132112","132115","132114","132122","132125","132111","132126","132118","132123","132120","132113","132119"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development Test of Inflatable Frame for Flexible Structure Atomospheric-entry"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-12","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"平成20年度","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"宇宙航行の力学シンポジウム(平成20年度)(2008年12月4～5日、宇宙航空研究開発機構宇宙科学研究本部)","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Symposium on Flight Mechanics and Astrodynamics 2008 (December 4-5, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A vehicle with a flexible aeroshell is promising for the innovative re-entry system because the aerodynamic heating during re-entry can be reduced dramatically due to its low-ballistic-coefficient.The key technologlies of this concept are the large, low-mass and flexible aeroshell. One of the solutions that satisfy these requirements is a flare-type flexible aeroshell sustain by an inflatable torus frame. Our group has researched various important subjects in order to apply the flexible aeroshell to actual atmospheric-entry missions. One topic of them is reported in this paper. The topic is a structural test of the flare-type inflatable aeroshell. The relation between the diferential pressure of inflatable torus and the maximum compressive force which inflatable torus is able to keep the configuration was obtained by the structural tests using two kinds of support rings. Furthermore, a low-speed wind tunnel test was carried out to investigate the configuration of inflatable aeroshell and its structural strength against anaerodynamic force during the night.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064729008","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)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"青山学院大学"},{"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"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部"},{"subitem_text_value":"東京大学大学院新領域創成科学研究科"},{"subitem_text_value":"東京大学大学院新領域創成科学研究科"},{"subitem_text_value":"青山学院大学"},{"subitem_text_value":"東海大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aoyama Gakuin University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (ISAS)(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (ISAS)(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Frontier Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Frontier Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Aoyama Gakuin University"},{"subitem_text_language":"en","subitem_text_value":"Tokai University"}]},"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":"木村, 裕介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 和彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"秋田, 大輔"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安部, 隆士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小山, 将史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 宏二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"林, 光一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"牧野, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kimura, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Kazuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akita, Daisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Abe, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koyama, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Kojiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayashi, A. Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makino, Hitoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"柔構造大気突入機用インフレータブルフレームの開発試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"柔構造大気突入機用インフレータブルフレームの開発試験"}]},"item_type_id":"5","owner":"1","path":["1664","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14431","relation_version_is_last":true,"title":["柔構造大気突入機用インフレータブルフレームの開発試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:34:38.199828+00:00"}