{"created":"2023-06-20T15:11:29.740573+00:00","id":41166,"links":{},"metadata":{"_buckets":{"deposit":"0aa827f1-4b61-4590-9090-3a28e587b056"},"_deposit":{"created_by":1,"id":"41166","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41166"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041166","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["450897","450898","450896","450893","450895","450899","450891","450894","450892","450890"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Arc-heating tests of thermal protection system materials for the H-2 rocket fairing"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"22","bibliographicPageStart":"1","bibliographicVolumeNumber":"1181","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"日本の次世代打ち上げ用ロケットH-2の頭部フェアリングに用いる熱防御システム(TPS)に適した材料をアーク加熱風洞により試験した。候補材料の主なものはエポキシ樹脂とシリコンゴムである。H-2ロケット上昇時の頭部空力加熱の最大値に合せて試験時加熱率は60〜100kW/平方メートルとした。試験結果によれば、TPS主材としては縮合型シリコンゴムが最適で、また、シリカコーティングは欠かすことのできないものである。また、フェアリング頭部の表面温度に関する試験と推算の結果から、熱防御のためのシリカコーティングの厚さは2mmで十分であると思われる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Materials suitable for the Thermal Protection System (TPS) of the rocket fairing for the Japanese next generation launch vehicle named H-2 were tested using an arc-heated wind tunnel. The main constituents of the candidate materials were epoxy resin and silicon rubber. The heating rate was from 60 to 100 kW/(sq m) in accordance with the maximum heating rate of the nose region of an ascending H-2 rocket. Test results showed that polycondensed silicon rubber was the best candidate as the main component of the TPS, and also that a SiC coating was indispensable. In addition, based on results and a preliminary estimation of the skin temperatures of the fairing nose region, a SiC coating of about two mm in thickness is considered sufficient to achieve thermal protection capability.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004196000","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: NAL TR-1181","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"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":"平林, 則明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松崎, 貴至"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福島, 幸夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 富久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 猛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirabayashi, Noriaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuzaki, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukushima, Yukio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Tomihisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Takeshi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01181.pdf","filesize":[{"value":"3.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01181.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41166/files/naltr01181.pdf"},"version_id":"70564e72-b31d-4ba0-9c60-0877593643df"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"断熱材料","subitem_subject_scheme":"Other"},{"subitem_subject":"耐熱材料","subitem_subject_scheme":"Other"},{"subitem_subject":"高温試験","subitem_subject_scheme":"Other"},{"subitem_subject":"エポキシ樹脂","subitem_subject_scheme":"Other"},{"subitem_subject":"熱特性","subitem_subject_scheme":"Other"},{"subitem_subject":"シリコンゴム","subitem_subject_scheme":"Other"},{"subitem_subject":"TPS","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防御性能試験","subitem_subject_scheme":"Other"},{"subitem_subject":"アーク加熱風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点熱伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点加熱率制御","subitem_subject_scheme":"Other"},{"subitem_subject":"熱吸収率","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"フェアリング","subitem_subject_scheme":"Other"},{"subitem_subject":"heat insurating material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat resisting material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high temperature test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat resistance characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"epoxy resin","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal property","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"silicon rubber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection capacity test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"arc heated 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":"stagnation point heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation point heating rate control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat absorption rate","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":"H-2ロケットフェアリング断熱材のアーク加熱試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"H-2ロケットフェアリング断熱材のアーク加熱試験"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41166","relation_version_is_last":true,"title":["H-2ロケットフェアリング断熱材のアーク加熱試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:49.196810+00:00"}