{"created":"2023-06-20T14:40:34.677232+00:00","id":7485,"links":{},"metadata":{"_buckets":{"deposit":"5bc4f7c5-b1c1-416c-803b-2232fd88a663"},"_deposit":{"created_by":1,"id":"7485","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7485"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007485","sets":["1543:1544:1556","1887:1891"]},"author_link":["39913","39914","39918","39917","39915","39916"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"次期小惑星探査ミッションはやぶさ2のミッション解析"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"298","bibliographicPageStart":"293","bibliographic_titles":[{"bibliographic_title":"第17回アストロダイナミクスシンポジウム講演後刷り集　2007"},{"bibliographic_title":"Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」のITOKAWA接近運用の結果を受け、次の小天体探査ミッションについては、他国に先駆けて、できるだけ早い時期に小天体からのサンプルリターンミッションを再実行する可能性を検討することとなった。ミッションは「はやぶさ2」と呼ばれ、探査機は開発期間短縮のために「はやぶさ」の設計をほぼ流用することになる。これにより、開発計画上は2010年度中に探査機を打ち上げられる見通しが立った。以上を受けて、本発表では「はやぶさ2」のミッションデザインの結果を報告する。2010年に打上げウィンドウがあり、「はやぶさ」同等の性能の探査機により実現可能な、科学的目的に合致する天体からのサンプルリターン、が「はやぶさ2」のミッションデザインの目標となる。発表では、探査対象天体の選定、ノミナルシーケンスの軌道計画、いくつかのバックアッププランについて報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Reported in this paper is the result of the mission analysis of the asteroid explorer mission. Following the results of Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft), the Japanese asteroid explorer, JAXA has started the study of the next asteroid exploration mission. The mission now under study gives priority on 'early' achievement of the sample return from an asteroid with primitive composition. Therefore, the design of the spacecraft follows that of Hayabusa basically as it is, and the spacecraft is planned to be launched in early 2010s. The objective of the mission analysis is to design a mission sequence, which has launch window in early 2010s, which is feasible by a Hayabusa-type spacecraft, and whose target asteroid complies with the science objective. The result includes the selection of the target asteroid, the design of nominal mission sequence, and some back up plans.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063718048","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/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"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":"川勝, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安部, 正真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川口, 淳一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawakatsu, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Abe, Masanao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawaguchi, Junichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"小惑星ミッション","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道解析","subitem_subject_scheme":"Other"},{"subitem_subject":"サンプルリターンミッション","subitem_subject_scheme":"Other"},{"subitem_subject":"小惑星","subitem_subject_scheme":"Other"},{"subitem_subject":"ミッション立案","subitem_subject_scheme":"Other"},{"subitem_subject":"はやぶさ2","subitem_subject_scheme":"Other"},{"subitem_subject":"低推力推進と地球スウィングバイ併用法","subitem_subject_scheme":"Other"},{"subitem_subject":"EDVEGA","subitem_subject_scheme":"Other"},{"subitem_subject":"ミッションシーケンス","subitem_subject_scheme":"Other"},{"subitem_subject":"推力プロフィル","subitem_subject_scheme":"Other"},{"subitem_subject":"推力","subitem_subject_scheme":"Other"},{"subitem_subject":"打上げウィンドウ","subitem_subject_scheme":"Other"},{"subitem_subject":"スイングバイ技術","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"asteroid mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sample return mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"asteroid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mission planning","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hayabusa2","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Electric Delta-V Earth Gravity Assist","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"EDVEGA","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mission sequence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust profile","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"launch window","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swingby technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transfer orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Mission analysis of Hayabusa 2, the next Japanese asteroid exploration mission","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Mission analysis of Hayabusa 2, the next Japanese asteroid exploration mission","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1556","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7485","relation_version_is_last":true,"title":["Mission analysis of Hayabusa 2, the next Japanese asteroid exploration mission"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:47.452174+00:00"}