{"created":"2023-06-20T14:36:01.319114+00:00","id":2321,"links":{},"metadata":{"_buckets":{"deposit":"c0942f20-2a56-450c-9f6e-b970d7aa90f8"},"_deposit":{"created_by":1,"id":"2321","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2321"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002321","sets":["1887:1893","9:10:309:321"]},"author_link":["5319","5320","5322","5318","5321","5323"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research and development of REV ablator in arc windtunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"75","bibliographicPageStart":"55","bibliographicVolumeNumber":"JAXA-RR-04-045","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告: USERS REVカプセルの開発研究および飛行後解析"},{"bibliographic_title":"JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"REV was the first reentry capsule developed through pure domestic technology and successfully recovered. REV is thermally protected against the severe aerodynamic heating by carbon-phenolic ablator material. The present paper describes the feature of the heating test in the arc wind tunnel and the ablator characteristics clarified during the research and development process of the REV heat shield. Because the heat flux anticipated on the stagnation surface is about 2 MW/sq m, the dominant surface recession mechanism is identified to be in the reaction control region. The thermochemical reaction data have been acquired through three arc-heater facilities with different enthalpy level for calibration and tuning of the ablation analysis code. The thermomechanical behavior of the ablator under the high heat flux environment such as delamination, or spallation also has been investigated for functional safety of the heat shield.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048710005","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-RR-04-045","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":"1349-1113","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":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"川崎重工業 航空宇宙カンパニー"},{"subitem_text_value":"川崎重工業 航空宇宙カンパニー"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd. Aerospace Company"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd. Aerospace Company"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"奥山, 圭一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 純郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 哲哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okuyama, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Sumio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Tetsuya","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":"48710005.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48710005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2321/files/48710005.pdf"},"version_id":"55e6604c-63d6-4c32-83ac-c8ba7a6bc9ed"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"アーク加熱風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"アブレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"リエントリモジュール","subitem_subject_scheme":"Other"},{"subitem_subject":"CFRP","subitem_subject_scheme":"Other"},{"subitem_subject":"USERSカプセル","subitem_subject_scheme":"Other"},{"subitem_subject":"USERSミッション","subitem_subject_scheme":"Other"},{"subitem_subject":"arc wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ablator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"recovery vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry module","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFRP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"USERS capsule","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"USERS mission","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":"アーク加熱風洞によるREVアブレータの研究開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"アーク加熱風洞によるREVアブレータの研究開発"}]},"item_type_id":"3","owner":"1","path":["321","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2321","relation_version_is_last":true,"title":["アーク加熱風洞によるREVアブレータの研究開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:24:40.102393+00:00"}