{"created":"2023-06-20T15:02:44.672033+00:00","id":31826,"links":{},"metadata":{"_buckets":{"deposit":"0bc59de5-d6a9-4861-8e3b-019fcff7adb0"},"_deposit":{"created_by":1,"id":"31826","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31826"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031826","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["406378","406379","406376","406380","406377","406381","406382","406375"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Rossibility of Structural Improvement of SSR-Rocket"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1966-06","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2_B","bibliographicPageEnd":"626","bibliographicPageStart":"622","bibliographicVolumeNumber":"2","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The small test rocket SSR, Which reached the altitude 25.8km in the latest flying test, is still possible to be improved from the structural point of view. From the results of the ground tests, the weight of some structual parts can be reduced and the reducible total weight is estimated about 30% of the total structural weight. It is shown that this weight reduction is also possible from the aeroelastic point of view. By this improvment, the increase of the maximum attainable altitude of SSR will be about 4. 7 km. Furthermore, this result is compared with the effects of aerodynamical improvement and of the improvement of the propellant.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124881000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"},{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"},{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"},{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"池田, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"富田, 文治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"古田, 敏康"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"酒巻, 正守"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IKEDA, Ken","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TOMITA, Bunji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FURUTA, Toshiyasu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SAKAMAKI, Masamori","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0124881.pdf","filesize":[{"value":"278.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124881.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31826/files/SA0124881.pdf"},"version_id":"8c5b3441-510e-4fc7-ac55-a01ca25fd159"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"II.1.9 構造の立場から見たSSRロケットの性能向上の可能性について(1 機体および構造)(II.関連研究)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"II.1.9 構造の立場から見たSSRロケットの性能向上の可能性について(1 機体および構造)(II.関連研究)"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31826","relation_version_is_last":true,"title":["II.1.9 構造の立場から見たSSRロケットの性能向上の可能性について(1 機体および構造)(II.関連研究)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:49:26.927100+00:00"}