{"created":"2023-06-20T15:02:54.038842+00:00","id":31989,"links":{},"metadata":{"_buckets":{"deposit":"d679e520-0df6-4681-8b03-5c6f7ee408f2"},"_deposit":{"created_by":1,"id":"31989","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31989"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031989","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["406905","406904","406902","406903"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Space environmental test of a thermos for space use"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1968-04","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2","bibliographicPageEnd":"279","bibliographicPageStart":"271","bibliographicVolumeNumber":"4","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":"アルミニウム製の三重の容器をつくり,その間に適当な熱絶縁を行なうことによって,内槽の温度変化を減少させる方式の恒温槽の試験を,スペース・シミュレーター中で行った.各槽間の熱的結合抵抗は,各槽間のふく射結合だけが存在するばあには,ほぼ計算どおりの値が得られたが,スーパーインシュレーション等をそう入して,より高度の熱絶縁を計っても,各種の漏洩抵抗のために,予期どおりの値は得られなかった.さらに,このような高度に熱絶縁された体系ではスペース・シミュレーター中に残留した分子の汚染効果による熱入力が影響して,内槽の温度は,予期していたより大きな変化を示すことがわかった.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A thermos, which is used aboard a spacecraft in order to maintain a constant temperature for a crystal oscillator, was environmentally tested in space simulators. This thermos is composed of three-fold aluminum containers, between which thermal insulation is applied. Measured thermal resistance between them showed reasonably consistent values with the calculated ones. However, the temperature of the inner container was seriously affected by contamination of residual gas molecule showing heavy drift and large cyclic variation. Thus the thermos for space use is recommended to be kept in pressurized vessel.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125070000","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"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中山, 晴美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大島, 耕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAYAMA, Harumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OSHIMA, Koichi","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":"SA0125070.pdf","filesize":[{"value":"516.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125070.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31989/files/SA0125070.pdf"},"version_id":"c2aacd70-f850-49ee-89cb-41df7cb580eb"}]},"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":"人工衛星搭載用恒温槽のスペース・シミュレーターによる性能試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"人工衛星搭載用恒温槽のスペース・シミュレーターによる性能試験"}]},"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":"31989","relation_version_is_last":true,"title":["人工衛星搭載用恒温槽のスペース・シミュレーターによる性能試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:44:24.729409+00:00"}