WEKO3
アイテム
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REV熱防御系の設計と飛行後解析
https://jaxa.repo.nii.ac.jp/records/2322
https://jaxa.repo.nii.ac.jp/records/23228b6b3075-1929-4a69-8d27-491545dd2e09
名前 / ファイル | ライセンス | アクション |
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48710006.pdf (3.2 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | REV熱防御系の設計と飛行後解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱防御システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リエントリモジュール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 回収機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アブレータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヒートシールド設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機再突入 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行後解析 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal protection system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry module | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | recovery vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ablator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat shield design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft reentry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | post-flight analysis | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Design and post-flight analysis of REV thermal protection system | |||||
著者 |
加藤, 純郎
× 加藤, 純郎× 菅野, 義就× 奥山, 圭一× 上垣, 栄一× 山田, 哲哉× 鈴木, 俊之× Kato, Sumio× Kanno, Yoshitsugu× Okuyama, Keiichi× Uegaki, Eiichi× Yamada, Tetsuya× Suzuki, Toshiyuki |
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著者所属 | ||||||
川崎重工業 航空宇宙カンパニー | ||||||
著者所属 | ||||||
川崎重工業 航空宇宙カンパニー | ||||||
著者所属 | ||||||
川崎重工業 航空宇宙カンパニー | ||||||
著者所属 | ||||||
川崎重工業 航空宇宙カンパニー | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. Aerospace Company | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. Aerospace Company | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. Aerospace Company | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. Aerospace Company | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
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 en : JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis 巻 JAXA-RR-04-045, p. 77-103, 発行日 2005-03-31 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The re-entry capsule USERS/REV was successfully recovered in May 2003. REV has a heat shield system to protect inner equipments against the severe heating environment during the re-entry. The heat shield system is mainly made of three kinds of layers, i.e., CFRP ablator, felt type insulation material with thermal anchor and an aluminum shell structure. In the design of the heat shield system, contradictory requirements of heat ejection in orbit and heat protection during the re-entry had to be satisfied. Thermal protection performance of the heat shield system was calculated using an ablation analysis code. Thermal stress analysis of the ablator during the reentry was carried out using a large deformation FEM that considers materials non-linearity. For the development of the heat shield system, various kinds of tests such as the arc-heated tests of the ablator and the strain survey test of the heat shield system were carried out. After the recovery of REV, evaluation of the recovered heat shield system was carried out. The temperature time histories in the ablator obtained during the re-entry and the damage of the heat shield system measured after the recovery were compared with the results of ablation analysis and structural analysis, from which the heating environment during the re-entry and the cause of the damage were estimated. The evaluation of the heat shield system design based on the flight results is also described. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048710006 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-04-045 |