アブレーション解析コードと飛行後解析

• 資料種別: 規格・テクニカルリポート類
• タイトル: アブレーション解析コードと飛行後解析
• 著者・編者: 加藤, 純郎; 奥山, 圭一; 山田, 哲哉; Kato, Sumio; Okuyama, Keiichi; Yamada, Tetsuya
• 著者標目: 加藤, 純郎; 奥山, 圭一; 山田, 哲哉; Kato, Sumio; Okuyama, Keiichi; Yamada, Tetsuya
• 出版事項: 宇宙航空研究開発機構
• 出版年月日等: 2005-03-31
• 出版年（W3CDTF）: 2005-03-31
• 並列タイトル等: Validation and post-flight analysis of the ablation analysis code
• タイトル（掲載誌）: 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 = JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis
• 巻号年月日等（掲載誌）: JAXA-RR-04-045
• 掲載巻: JAXA-RR-04-045
• 掲載ページ: 31-54
• ISSN（掲載誌）: ISSN : 1349-1113
• 本文の言語コード: jpn
• 件名標目: 宇宙機再突入; USERSカプセル; アブレーション解析コード; 計算機プログラム; 空力加熱; 熱防御; 数学モデル; アブレーション; CFRP; 飛行後解析; spacecraft reentry; USERS capsule; ablation analysis code; computer program; aerodynamic heating; thermal protection; mathematical model; ablation; post-flight analysis
• 対象利用者: 一般
• 一般注記: 出版タイプ： NA; A computer code for charring ablation and thermal response analysis has been developed for simulation of one-dimensional transient thermal behavior of multi-layer stack of isotropic charring ablation materials used for re-entry capsules. A mathematical model of charring ablation including governing equations is summarized. Analytical solutions of several thermal response problems with or without ablation agreed very well with numerical results that are obtained with the charring ablation analysis code. Arc-heated tests of CFRP ablator models were carried out and measured results including temperature response data were compared with the simulation results of the ablation analysis code. The test results and the simulation results agreed very well. Measurements of the successfully recovered USERS/REV ablator were carried out. The measured results of the in-depth temperature history in the ablator, the char depth, the surface recession, etc. agreed well with the simulation results using the ablation analysis code. These results show that the ablation analysis code based on the present mathematical model are available for the thermal response prediction of CFRP ablator used in the re-entry capsules such as USERS/REV.; 資料番号: AA0048710004; レポート番号: JAXA-RR-04-045
• 掲載誌（NCID）: AA1192675X; https://ci.nii.ac.jp/ncid/AA1192675X
• 連携機関・データベース: 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）; https://irdb.nii.ac.jp
• 提供元機関・データベース: 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ