{"created":"2023-06-20T15:03:26.239273+00:00","id":32647,"links":{},"metadata":{"_buckets":{"deposit":"5f3c8f74-276e-4da8-8ca8-92d5c180c60c"},"_deposit":{"created_by":1,"id":"32647","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32647"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032647","sets":["1887:1890","1896:1898:1899:1911"]},"author_link":["410543","410546","410544","410541","410545","410547","410550","410539","410540","410542","410548","410549"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Trajectory dispersion of the Viper caused by the elastic vibration"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"34","bibliographicPageStart":"1","bibliographicVolumeNumber":"100","bibliographic_titles":[{"bibliographic_title":"宇宙科学研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告では, 発射時に生じるロケット本体及びランチャーの弾性振動に起因する Viper ロケットの軌道分散について報告する。軌道分散の推定のために, ロケット及びランチャーの弾性を考慮した発射の三次元数値シミュレーションを行なった。実際の発射時に計測された振動データとの比較によりシミュレーションの精度を確認した後に, シミュレーションを用いて軌道分散の推定を行なった。その結果, 弾性振動に起因する軌道分散は実際の打ち上げミッションにおいて問題にならない値であることが確認された。","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, the trajectory dispersion of the Viper rocket caused by the elastic vibration of the vehicle and rocket launcher is investigated. In order to estimate the trajectory dispersion, a three dimensional numerical simulation of the launch was carried out considering the elastical effect of the vehicle and rocket launcher. The accuracy of the numerical simulation was validated first by the comparison with the vibration data measured on actual launch, and after that the trajectory dispersion was estimated by the simulation. As the result, it is confirmed that the trajectory dispersion caused by th elastic vibration is no matter on actual launch mission.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0165943000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0285-2853","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":"AN00354474","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学大学院工学系研究科航空宇宙工学専攻"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"竹内, 伸介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野田, 淳次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"峯杉, 賢治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋元, 保雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"富沢, 利夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"下瀬, 滋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKEUCHI, Shinsuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ONODA, Junjiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MINESUGI, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASHIMOTO, Yasuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TOMIZAWA, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMOSE, Shigeru","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":"SA0165943.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0165943.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32647/files/SA0165943.pdf"},"version_id":"cd1afbde-0a37-4105-bf99-a0e22cf2e2b5"}]},"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":"弾性振動に起因する Viper ロケットの軌道分散","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"弾性振動に起因する Viper ロケットの軌道分散"}]},"item_type_id":"9","owner":"1","path":["1890","1911"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32647","relation_version_is_last":true,"title":["弾性振動に起因する Viper ロケットの軌道分散"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:27:12.043389+00:00"}