{"created":"2023-06-20T15:10:16.593574+00:00","id":39865,"links":{},"metadata":{"_buckets":{"deposit":"9ac3a36c-ede1-4ed0-a0ee-87dc9c2a0911"},"_deposit":{"created_by":1,"id":"39865","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39865"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039865","sets":["1887:1893","1896:1898:1933:1934"]},"author_link":["500731","500730","500735","500725","500724","500729","500726","500736","500727","500728","500734","500737","500738","500739","500733","500732"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Observation of flow condition in capillary pump loop under microgravity environment"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"17","bibliographicPageStart":"11","bibliographic_titles":[{"bibliographic_title":"宇宙開発事業団技術報告"},{"bibliographic_title":"NASDA Technical Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"スペースステーションやスペースプラットホームのような大型で複雑な宇宙機に対して2相熱制御システムの適用が期待されている。将来大型宇宙機ミッションが予定される状況下で、流体顕熱だけからなる各種のサーマルループが、有望な高出力熱管理装置であると考えている。CPL(キャピラリポンプループ)は蒸発および凝縮の潜熱を利用する熱輸送装置である。通常の機械的2相熱輸送システムよりも長距離にわたって大量の熱を輸送することができる。本論文は、蒸発器、凝縮器およびアイソレータ内部の蒸気と液体の流れ分布、および熱伝達能力について実験結果を述べた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The application of two phase thermal control systems is anticipated for large and complex spacecraft such as space station and space platforms. Under these circumstances of future large scale spacecraft mission, various kinds of thermal loop with only sensible fluid heat are considered as promising devices for high power thermal management. The CPL (Capillary Pump Loop) is a heat transfer device which employs the latent heat of vaporization and condensation. It can transfer large amounts of heat over longer distances than conventional mechanical two phase heat transfer system. This paper describes the experimental results which are flow patterns of vapor and liquid inside the evaporator, condenser and isolator, and heat transfer capability.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000742002","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: NASDA-TMR-960025","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙開発事業団"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Space Development Agency of Japan (NASDA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1345-7888","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":"AN00364784","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙環境利用推進センター"},{"subitem_text_value":"日本電気"},{"subitem_text_value":"日本電気"},{"subitem_text_value":"日本電気"},{"subitem_text_value":"NEC航空宇宙システム"},{"subitem_text_value":"早稲田大学"},{"subitem_text_value":"早稲田大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"Japan Space Utilization Promotion Center"},{"subitem_text_language":"en","subitem_text_value":"NEC Corporation"},{"subitem_text_language":"en","subitem_text_value":"NEC Corporation"},{"subitem_text_language":"en","subitem_text_value":"NEC Corporation"},{"subitem_text_language":"en","subitem_text_value":"NEC Aerospace Systems Ltd"},{"subitem_text_language":"en","subitem_text_value":"Waseda University"},{"subitem_text_language":"en","subitem_text_value":"Waseda University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石井, 誠一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石倉, 精三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 清志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"間瀬, 一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 源四郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮崎, 慈"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永田, 勝也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"勝田, 正文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishii, Seiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikura, Seizo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Kiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mase, Ichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Genshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazaki, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagata, Katsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katsuta, Masafumi","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":"2020-02-10"}],"displaytype":"detail","filename":"00742002.pdf","filesize":[{"value":"332.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"00742002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39865/files/00742002.pdf"},"version_id":"9cefc952-f4df-4ab6-a873-63e336b0b5ff"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"MU-300型航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"パラボリックフライト","subitem_subject_scheme":"Other"},{"subitem_subject":"微小重力環境","subitem_subject_scheme":"Other"},{"subitem_subject":"CPL","subitem_subject_scheme":"Other"},{"subitem_subject":"キャピラリポンプループ","subitem_subject_scheme":"Other"},{"subitem_subject":"2相熱輸送","subitem_subject_scheme":"Other"},{"subitem_subject":"潜熱","subitem_subject_scheme":"Other"},{"subitem_subject":"顕熱","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースステーション","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプラットホーム","subitem_subject_scheme":"Other"},{"subitem_subject":"蒸発器","subitem_subject_scheme":"Other"},{"subitem_subject":"凝縮器","subitem_subject_scheme":"Other"},{"subitem_subject":"フレオン","subitem_subject_scheme":"Other"},{"subitem_subject":"アイソレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"MU 300 aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parabolic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microgravity environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CPL","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"capillary pump loop","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two phase heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"latent heat","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sensible heat","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space station","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space platform","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"evaporator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"condenser","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"freon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"isolator","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":"微小重力下でのcapillary pump loopの作動実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"微小重力下でのcapillary pump loopの作動実験"}]},"item_type_id":"3","owner":"1","path":["1893","1934"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39865","relation_version_is_last":true,"title":["微小重力下でのcapillary pump loopの作動実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T20:28:33.125031+00:00"}