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Thermal Response Simulation of Ultra Light Weight Phenolic Carbon Ablator by the Use of the Ablation Analysis Code
http://hdl.handle.net/10228/00007622
http://hdl.handle.net/10228/00007622d108cc75-046c-4d2d-af48-4552f11919f7
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2012_03.pdf (1.3 MB)
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| Item type | 学術雑誌論文 = Journal Article(1) | |||||
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| 公開日 | 2020-02-19 | |||||
| 資源タイプ | ||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
| 資源タイプ | journal article | |||||
| タイトル | ||||||
| タイトル | Thermal Response Simulation of Ultra Light Weight Phenolic Carbon Ablator by the Use of the Ablation Analysis Code | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 著者 |
Kato, Sumio
× Kato, Sumio× Okuyama, Kei-ichi× Gibo, Kenta× Miyagi, Takuma× Suzuki, Toshiyuki× Fujita, Kazuhisa× Sakai, Takeharu× Nishio, Seiji× Watanabe, Akihiro |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield system to protect inner equipments against severe aerodynamic heating environments. Charring ablator is usually used for the heat shield system. In order to design the heat shield system, it is necessary to predict the thermal behavior under aerodynamic heating by ablation analysis. A computer code for charring ablation and thermal response analysis is newly developed for simulation of one-dimensional transient thermal behavior of charring ablation materials. The mathematical model for the charring ablation including basic equation and computational method of ablation analysis is briefly described. A new ultra light weight phenolic carbon ablator called LATS (Lightweight Ablator series for Transfer vehicle) was recently developed. Arc-heated tests of the LATS ablator were carried out and measured results of the temperature response and surface mass loss are compared with the simulation results of the ablation analysis program. The agreement between the results of simulation and measurement is found to be good. It is also found that the mathematical model used in the ablation code can be applied to the ablation analysis of the low density LATS ablator. | |||||
| 言語 | en | |||||
| 備考 | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | 28th International Symposium on Space Technology and Science (28th ISTS), 5-12 June 2011, Okinawa, Japan | |||||
| 書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 10, 号 ists28, p. Pe_31-Pe_39, 発行日 2012-08-15 |
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| 出版社 | ||||||
| 出版者 | 日本航空宇宙学会 | |||||
| DOI | ||||||
| 関連タイプ | isIdenticalTo | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | https://doi.org/10.2322/tastj.10.Pe_31 | |||||
| ISSN | ||||||
| 収録物識別子タイプ | EISSN | |||||
| 収録物識別子 | 1884-0485 | |||||
| 著作権関連情報 | ||||||
| 権利情報 | Copyright (c) 2012 The Japan Society for Aeronautical and Space Sciences | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Ablator | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Heat Shield System | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Re-entry Capsule | |||||
| 出版タイプ | ||||||
| 出版タイプ | VoR | |||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
| 査読の有無 | ||||||
| 値 | yes | |||||
| 連携ID | ||||||
| 値 | 7988 | |||||
