{"created":"2023-06-20T15:07:29.216265+00:00","id":36856,"links":{},"metadata":{"_buckets":{"deposit":"6de0880a-36b0-4c01-892a-bb63878736e3"},"_deposit":{"created_by":1,"id":"36856","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36856"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036856","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477887","477888"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Thermal protection system evaluation with the flight data"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"162","bibliographicPageStart":"151","bibliographicVolumeNumber":"32","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HYFLEX(極超音速飛行実験)機の熱防護系の機能を飛行データに基づいて評価した。各センサの計測は良好に行われ、飛行実験中の各材料の最高温度は許容上限以下であったことが確認された。熱防護系の構成、計測項目および得られた飛行データの概要を示す。また、計測点のうちのいくつかについて実飛行環境に基づく再計算との比較を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Thermal protection system of the HYFLEX (Hypersonic Flight Experiment) vehicle is evaluated with the flight data. Every sensor worked well in flight measurement. Flight data shows that the measured maximum temperatures were under allowable limits for each materials. Explanation of the thermal protection system summary of the flight data, and examples of post flight analysis using measured heating rates are shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000584018","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-32","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙開発事業団"}]},"item_5_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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"甲斐, 高志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kai, Takashi","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":"nalsp0032018.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0032018.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36856/files/nalsp0032018.pdf"},"version_id":"9a1a032e-cd8d-460c-b7c7-2412e5b5222a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防護系","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"性能評価","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行データ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"複合材料","subitem_subject_scheme":"Other"},{"subitem_subject":"炭素","subitem_subject_scheme":"Other"},{"subitem_subject":"セラミックタイル","subitem_subject_scheme":"Other"},{"subitem_subject":"可撓断熱材","subitem_subject_scheme":"Other"},{"subitem_subject":"ノーズキャップ","subitem_subject_scheme":"Other"},{"subitem_subject":"エレボン","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移","subitem_subject_scheme":"Other"},{"subitem_subject":"加熱比","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFELX vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight data analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"composite material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ceramic tile","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flexible surface insulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nose cap","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elevon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heating ratio","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"飛行データに基づいた熱防護系の評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"飛行データに基づいた熱防護系の評価"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36856","relation_version_is_last":true,"title":["飛行データに基づいた熱防護系の評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:32.068909+00:00"}