{"created":"2023-06-20T14:40:31.888252+00:00","id":7427,"links":{},"metadata":{"_buckets":{"deposit":"b9bdd9a4-fd4b-419e-b566-9c7cd6680853"},"_deposit":{"created_by":1,"id":"7427","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7427"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007427","sets":["1543:1544:1555","1887:1891"]},"author_link":["39480","39483","39484","39486","39485","39481","39482","39487"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Analysis of Tether Deployment for the Sounding Rocket Experiment"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"2008","bibliographic_titles":[{"bibliographic_title":"アストロダイナミクスシンポジウム講演後刷り集"},{"bibliographic_title":"Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics","bibliographic_titleLang":"en"}]}]},"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 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"摘要: S520-25th T-Rex の最も重要な目標の一つがフリーフライング衛星を用いたテザーの高速伸展である。衛星の姿勢は本体の機軸周りのスピンと機軸外残留角速度によるニューテーションと固体燃料タンク内部の残留燃料による残留推力の影響を受け、不安定となる恐れがある。テザー進展中のニューテーション運動をする衛星の運動を３次元剛体の運動として取り扱い、それらが衛星の運動に影響を決定するために以下の２つの条件におけるシミュレーションを行う。1) 残留推力を無視した場合2) 残留推力がある場合また、数値シミュレーションの精度を微小重力実験とシミュレーションの結果を比較することで行った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"One of the most important objectives for the S520-25th T-REx (stands for Tethered-sounding Rocket Experiment) is a high speed tether deployment with free-flying space tethered satellites. Attitude of the satellite can be unstable due to nutation induced by interaction of on-axis spin and off-axis angular velocity and a residual thrust caused by slivers remaining in a solid propellant tank. Dynamic behavior of the nutating satellite during deployment of tether is studied in terms of 3-dimensional dynamic behavior of a rigid body and is simulated numerically to determine how they affect the dynamic behavior of the satellite under the following situations.1) When the residual thrust is negligible2) When the residual thrust is not negligibleComparison analysis is also discussed in order to evaluate the accuracy of the numerical simulations by comparing the results of the numerical simulations and with microgravity experiments.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064733053","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_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11567475","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"首都大学東京"},{"subitem_text_value":"首都大学東京"},{"subitem_text_value":"首都大学東京"},{"subitem_text_value":"神奈川工科大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Kanagawa Institute of Technology"}]},"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":"杉本, 洋平"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小島, 広久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡部, 武夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 裕矩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugimoto, Yohei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kojima, Hirohisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Hironori A.","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":"観測ロケット実験におけるテザー伸展の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"観測ロケット実験におけるテザー伸展の数値解析"}]},"item_type_id":"5","owner":"1","path":["1555","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7427","relation_version_is_last":true,"title":["観測ロケット実験におけるテザー伸展の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:39:41.716146+00:00"}