{"created":"2023-06-20T14:36:21.176237+00:00","id":2666,"links":{},"metadata":{"_buckets":{"deposit":"9e1e3e96-f8a1-444c-93f0-8be327c1a648"},"_deposit":{"created_by":1,"id":"2666","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2666"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002666","sets":["1887:1893","9:1090:1311:1323"]},"author_link":["8152","8151","8155","8156","8153","8154"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A study of the space energy utilization: Solar power satellite system configured by formation flying"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-10-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"7","bibliographicVolumeNumber":"JAXA-RM-04-011","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:先行研究等"},{"bibliographic_title":"JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Advanced Technology","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents a new concept of a solar power satellite system configured by formation flying (Formation-Flying Solar Power Satellite: FF-SPS). In this concept, the solar power satellite system consists of sunlight reflectors and an Earth-pointing segment. The Earth-pointing segment is on a common GEO, and the reflectors are placed on the north and south by using solar pressure to raise their orbits from GEO. Therefore, the orbits of the reflectors and that of the Earth-pointing segment make three parallel GEOs. The feasibility is also discussed focusing on the orbital and attitude mechanics of the reflector. Through some analyses, it is shown that the required propellant for the control of the formation flying SPS is about a few 10 percent larger than that for previous concepts. The structural feasibility is also discussed through FEM analyses. It is revealed that it is possible to assemble the lightweight reflector structure with sufficient stiffness using deployable structures based on current technologies. Although FF-SPS requires more control propellant than previous concepts, its feasibility is technologically equivalent to previous ones. FF-SPS is the first concept that has both Earth-pointing and Sun-pointing segments without any single point of failure.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048129002","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-04-011","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_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 Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"武市, 昇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上野, 浩史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小田, 光茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takeichi, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueno, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oda, Mitsushige","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":"48129002.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48129002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2666/files/48129002.pdf"},"version_id":"0a8530a3-2b2b-4d26-939c-786a328b18dc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙エネルギー利用","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽発電","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽光","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽発電衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"編成飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"反射板","subitem_subject_scheme":"Other"},{"subitem_subject":"FEM","subitem_subject_scheme":"Other"},{"subitem_subject":"マイクロ波","subitem_subject_scheme":"Other"},{"subitem_subject":"space energy utilization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar generator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sunlight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar power satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"formation flying","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reflector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FEM","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microwave","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"宇宙エネルギー利用システムの研究:フォーメーションフライトにより構成されるSSPS","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"宇宙エネルギー利用システムの研究:フォーメーションフライトにより構成されるSSPS"}]},"item_type_id":"3","owner":"1","path":["1323","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2666","relation_version_is_last":true,"title":["宇宙エネルギー利用システムの研究:フォーメーションフライトにより構成されるSSPS"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:18:17.740354+00:00"}