{"created":"2023-06-20T15:02:58.134563+00:00","id":32050,"links":{},"metadata":{"_buckets":{"deposit":"f9694fca-08db-4b2f-b8b3-fd8238840a02"},"_deposit":{"created_by":1,"id":"32050","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32050"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032050","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["407093","407092","407091","407094"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Solar Panel's Power of The Satellite No.1"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1969-01","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1A","bibliographicPageEnd":"79","bibliographicPageStart":"61","bibliographicVolumeNumber":"5","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"1号科学衛星のフライトユニット1号(以下F_1と略記)用太陽電池パネルの出力について,パネルの温度分布,入射角依存性とスピンによる影響を考慮して計算を行なった.また地上テストによる実測換算値と比較検討を試みた.その結果気象条件の変動などに対する厳密な補正が残されているとはいえ,本衛星は,計算値との一致が比較的よいことから,まず放射線損傷を無視した場合Air Mass Zero(以下AMOと略記)の太陽光強度140mW/cm^2, 20～30℃の温度範囲で,パネル出力約30Wが可能となった.すなわちダイオード損失,放射線損失を考慮した1例として入射角0°の赤道照射で約12Wが負荷電力として供給し得るであろう.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The power output from the solar cell panels of Flight Unit No.1 of the scientific satellite No.1 (M-4 S-1-F_1) is discussed. The calculations are developed, including the effect of an operational temperature and a spin on the panel's output. Finally their results are compared with those of outdoor sunlight test. As a result, measured values were considerably consistent with calculated ones. Therefore, in the case of insolance of 140mW/cm^2 at Air Mass Zero, the solar panels can supply about 30 watts on the output side of the panels in the temperature range of 20～30℃, and also about 12 watts to the load on the output side of the switching type regulators under the equatorial illumination, if the losses caused by one year's radiation damage and the potential drop across the blocking diodes are assumed to be 3.3 watts.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125144000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所宇宙工学"},{"subitem_text_value":"東京大学宇宙航空研究所宇宙工学"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"後川, 昭雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, 慶治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"USHIROKAWA, Akio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKAHASHI, Keiji","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0125144.pdf","filesize":[{"value":"2.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125144.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32050/files/SA0125144.pdf"},"version_id":"32949dc7-b241-4ed5-91d7-f969b91469a1"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"<研究報告>1号科学衛星の太陽電池出力","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"<研究報告>1号科学衛星の太陽電池出力"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32050","relation_version_is_last":true,"title":["<研究報告>1号科学衛星の太陽電池出力"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:42:35.919163+00:00"}