{"created":"2023-06-20T15:02:45.873712+00:00","id":31845,"links":{},"metadata":{"_buckets":{"deposit":"99820d05-a571-4076-8422-80e68a4958fa"},"_deposit":{"created_by":1,"id":"31845","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31845"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031845","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["406484","406482","406481","406485","406483","406480"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flight Performance 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":"825","bibliographicPageStart":"818","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":"In this report, the flight performances of SSR Rockets, HT-110-1, 2 and 3, under the condition of no cross wind are analysed. These three rockets have slightly different characteristics in total weight, configuration and weight of payload except the engine performance. The calculational results show that the maximum altitudes of trajectories of these rockets are about 20～27km when the launching angle is 70°, and that fairly good coincidence with the results of flight testing, hence especially the adequancy of evaluation of drag coefficients, which will be considered mainly to affect the performance of small rockets such as HT-110 types, was corroborated.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124900000","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":"三菱重工業K.K.名古屋航空機製作所"},{"subitem_text_value":"三菱重工業K.K.名古屋航空機製作所"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"富田, 文治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小早川, 眞也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"酒井, 春雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TOMITA, Bunji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KOBAYAKAWA, Shinya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SAKAI, Haruo","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":"SA0124900.pdf","filesize":[{"value":"344.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124900.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31845/files/SA0124900.pdf"},"version_id":"1ba665c8-f223-4f8e-898e-1cc688e6ff09"}]},"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.5.1 飛しょう性能(5 性能および気道)(II.関連研究)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"II.5.1 飛しょう性能(5 性能および気道)(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":"31845","relation_version_is_last":true,"title":["II.5.1 飛しょう性能(5 性能および気道)(II.関連研究)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:48:52.204732+00:00"}