{"created":"2023-06-20T14:38:16.449271+00:00","id":4788,"links":{},"metadata":{"_buckets":{"deposit":"faea5c74-9010-4307-b3c0-31d607b6a19c"},"_deposit":{"created_by":1,"id":"4788","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4788"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004788","sets":["1398:1501:1506","1543:1827:1832","1887:1891","9:789:920:926"]},"author_link":["21843","21847","21844","21838","21846","21839","21840","21837","21845","21834","21833","21836","21848","21841","21842","21835"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research on electrodynamic tether system for debris 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(JAXA))","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"有効なデブリ除去システム実現のためには､低コストで簡素な軌道変換用推進系が必要となる。候補となる推進系は､除去対象デブリの大きさや軌道等の条件により様々だが､本研究では小型衛星サイズ以上の低軌道高度デブリの軌道変換に有効と考えられる導電性テザー(EDY)を研究対象とする。EDTは､導電性のワイヤ(テザー)を軌道上で展開して電流を流すことで､電流と地球磁場との相互作用により生じるローレンツ力を推進力として利用する。その最大の長所は推進剤を必要としない点であり､自己誘導準起電力により電流を駆動できるため､軌道降下DeltaⅤの発生に要する消費電力も小さい。さらに､通常の推進系と異なり推力方向制御が不要なため､非協力物体の軌道変換に適する。JAXA研究開発本部では､このEDT技術を獲得するため､軌道上実証実験に向けてテザーや分離機構､リール､電子源なとの主要機器の研究開発を進めてきた。本発表ではその現状を報告する。","subitem_description_type":"Abstract"}]},"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 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Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Spacecraft Structures and Mechanisms Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Spacecraft Structures and Mechanisms Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"大川, 恭志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河本, 聡美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"北村, 正治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"東出, 真澄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上村, 平八郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木部, 勢至朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松本, 康司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塩見, 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