{"created":"2023-06-20T15:02:16.318296+00:00","id":31359,"links":{},"metadata":{"_buckets":{"deposit":"5f0e9fd9-b5d1-4bbf-9ce9-0c7ebc09c4ae"},"_deposit":{"created_by":1,"id":"31359","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31359"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031359","sets":["1887:1890","1896:1898:1899:1903"]},"author_link":["404098","404093","404097","404095","404094","404096"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1982-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"19","bibliographicPageStart":"1","bibliographicVolumeNumber":"601","bibliographic_titles":[{},{"bibliographic_title":"The Institute of Space and Astronautical Science report","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Two axially grooved heat pipes, one using ammonia as the working fluid and another using freon 11,were launched aboard S-520 sounding rockets in January 1980 and in September 1981,respectively. The former was made of aluminum and the latter of aluminum alloy. N-eicosane was employed as a phase change heat sink material for both cases. They were fixed on the rocket axis with the condenser top. The heat pipes experienced several levels of varying acceleration such as large positive during the boosting period, small negative immediately after the burnout caused by the aerodynamic drag on the rocket, zero-gravity, and again positive while the re-entry. They responded to these situations. Such responses as dryout, recovery from the dryout with partial liquid blockage in the condenser section, and resumption of normal heat pipe operation were resulted from the dynamic behavior of the working fluid. The flight data were analyzed to understand the heat pipe performance and to investigate the dependence of the liquid motion on the body force and on the surface tension. The critical Bond number which gave a boundary between surface tension dominating and body force dominating regions was found to be the order of 10^-3","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0034916000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0285-6808","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":"AA10632072","subitem_source_identifier_type":"NCID"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Structural Engineering, University of Tsukuba."},{"subitem_text_language":"en","subitem_text_value":"Institute of Structural Engineering, University of Tsukuba."},{"subitem_text_language":"en","subitem_text_value":"NEC Nippon Electric Co., Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Nippon Electric Co., Ltd."},{"subitem_text_language":"en","subitem_text_value":"NEC Nippon Electric Co., Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"MURAKAMI, Masahide","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TADEUCHI, Ryo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HAYASHI, Tomonao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MACHIDA, Tsuneo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KATO, Seiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATSUFUJI, Yukio","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0034916.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0034916.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31359/files/SA0034916.pdf"},"version_id":"25c0dcda-ae0d-449e-b3b3-dbf8d4fc5b84"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Thermal Behavior of Axially Grooved Heat Pipes aboard a Rocket","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Thermal Behavior of Axially Grooved Heat Pipes aboard a Rocket","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1903"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31359","relation_version_is_last":true,"title":["Thermal Behavior of Axially Grooved Heat Pipes aboard a Rocket"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T01:02:11.451831+00:00"}