{"created":"2023-06-20T14:36:31.441711+00:00","id":2838,"links":{},"metadata":{"_buckets":{"deposit":"e6bdd513-04be-43ce-9424-d635bd371305"},"_deposit":{"created_by":1,"id":"2838","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2838"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002838","sets":["1398:1501:1502","1543:1827:1828","1887:1891","9:789:794:795"]},"author_link":["9216","9210","9214","9212","9211","9217","9208","9215","9209","9213"],"item_4_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"デブリ除去に必要な要素技術の実証衛星とシステム実証衛星の実現性検討"}]},"item_4_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2019-03-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"437","bibliographicPageStart":"427","bibliographicVolumeNumber":"JAXA-SP-18-011","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第8回スペースデブリワークショップ講演資料集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 8th Space Debris Workshop","bibliographic_titleLang":"en"}]}]},"item_4_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第8回スペースデブリワークショップ (2018年12月3-5日. 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC)), 調布市, 東京","subitem_description_type":"Other"}]},"item_4_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":"The 8th Space Debris Workshop (December 3-5, 2018. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC)), Chofu, Tokyo, Japan","subitem_description_type":"Other"}]},"item_4_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"近年、スペースデブリの増加が大きな問題として認識されており、解決策の一つとしてデブリを積極的に除去するデブリ除去衛星の研究がなされている。特に、混雑軌道にあるロケット上段は、衝突時の影響が大きいことから、除去対象のデブリとして検討がなされている。当社は、デブリ除去の方法として、導電性テザー（EDT）を使用した方法を提案している。これは、デブリ除去衛星により、ロケット上段のPAF 開口部にEDT を取り付け、軌道遷移させる方法である。この方法では、非協力ターゲットであるロケット上段への接近技術、EDT を取り付けるための捕獲技術、EDT による減速技術の3つのキーとなる要素技術がある。それぞれの要素技術には技術的課題があるため、各技術の軌道上実証をした上でデブリ除去衛星のシステム実証へ進むことで、デブリ除去衛星の早期かつ低コストでの実現が期待できる。本発表では、デブリ除去に必要な要素技術の軌道上実証を目的とした超小型衛星と、システム実証を目的とした小型衛星のシステム検討結果について発表する。なお、デブリ除去の要素技術実証のため、当社で独自開発中の超小型衛星「DRUMS」についても紹介する。","subitem_description_type":"Abstract"}]},"item_4_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Recently, a growth of space debris has been recognized as a significant problem and Active Debris Removal (ADR) has been studied as one of the solution for it. To remove upper stages of rocket in congestion orbit is most effective because of it is large volume and mass, so it is considered as one of the targets for ADR mission. Kawasaki Heavy Industries proposes ADR mission which uses Electrodynamic tether (EDT) attached on PAF (Payload Attachment Fitting) of the upper stage of rocket. In this mission, there are three key technologies, 'non-cooperative rendezvous', 'capturing PAF' and 'deorbit by EDT'. However each technology has technical problems and it is difficult to verify them on the ground. So it is necessary to verify them in orbit as a step for ADR satellite. This paper describes the satellite system studies for verifying the key technologies and ADR system. It also describes Kawasaki Heavy Industries' micro size satellite 'DRUMS ; Debris Removal Unprecedented Micro-Satellite' used for verification of ADR key technologies.","subitem_description_type":"Other"}]},"item_4_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_4_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_4_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1830034034","subitem_description_type":"Other"}]},"item_4_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-18-011","subitem_description_type":"Other"}]},"item_4_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_4_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_4_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2232","subitem_source_identifier_type":"ISSN"}]},"item_4_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"川崎重工業株式会社"},{"subitem_text_value":"川崎重工業株式会社"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_4_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries, Ltd."},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries, Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中本, 浩樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"丸山, 辰也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岡本, 博之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河本, 聡美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山元, 透"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamoto, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maruyama, Tatsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okamoto, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawamoto, Satomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Toru","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":"2020-01-15"}],"displaytype":"detail","filename":"AA1830034034.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1830034034.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2838/files/AA1830034034.pdf"},"version_id":"bcb52e5a-9d50-4ce1-b789-0fe07df00668"}]},"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 object","resourceuri":"http://purl.org/coar/resource_type/c_c94f"}]},"item_title":"Feasibility Study of Active Debris Removal Satellite for Key Technology Demonstration and System Demonstration","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Feasibility Study of Active Debris Removal Satellite for Key Technology Demonstration and System Demonstration","subitem_title_language":"en"}]},"item_type_id":"4","owner":"1","path":["795","1502","1828","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-03-15"},"publish_date":"2019-03-15","publish_status":"0","recid":"2838","relation_version_is_last":true,"title":["Feasibility Study of Active Debris Removal Satellite for Key Technology Demonstration and System Demonstration"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:15:16.393658+00:00"}