WEKO3
アイテム
Thermochemical Performance of a Lightweight Charring Carbon Fiber Reinforced Plastic
http://hdl.handle.net/10228/00007621
http://hdl.handle.net/10228/000076214d12f406-40e7-4a34-bf34-370195729f4e
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2012_05.pdf (799.8 kB)
|
|
| Item type | 学術雑誌論文 = Journal Article(1) | |||||
|---|---|---|---|---|---|---|
| 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 | Thermochemical Performance of a Lightweight Charring Carbon Fiber Reinforced Plastic | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 著者 |
Okuyama, Keiichi
× Okuyama, Keiichi× Kato, Sumio× Ohya, Hiroaki |
|||||
| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | A new class of lightweight carbon fiber reinforced plastic (CFRP)–-the lightweight ablator series for transfer vehicle systems (LATS)–-has recently been developed. The LATS is fabricated by heating and pressurizing a material in which resin is impregnated in the laminated carbon fiber felt. A characteristic required to ensure the excellence of a conventional lightweight CFRP ablator of the LATS is the simplicity of the resin impregnation process. Since dried bulk density can be easily controlled, this manufacturing method is beneficial for use in the aerospace industry. Here, the ablation characteristics of this material under high-enthalpy airflow are described by a recently developed computer code to simulate the one-dimensional transient thermal behavior. The validity of the mathematical model and the applicability of the ablation code are then discussed by comparing the simulated and experimental results of arc-heated tests with the LATS. A new index adopted in this study predicted the mass loss rate; the measured and estimated values of the total mass loss rate in various test conditions are in good agreement. Thus, a heated LATS material shows excellent performance characteristics for use in re-entry vehicles, and its surface and in-depth temperatures can be estimated using the developed analysis code. | |||||
| 言語 | en | |||||
| 書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences 巻 56, 号 3, p. 159-169 |
|||||
| 出版社 | ||||||
| 出版者 | 日本航空宇宙学会 | |||||
| 言語 | ja | |||||
| DOI | ||||||
| 関連タイプ | isIdenticalTo | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | https://doi.org/10.2322/tjsass.56.159 | |||||
| 日本十進分類法 | ||||||
| 主題Scheme | NDC | |||||
| 主題 | 578 | |||||
| NCID | ||||||
| 収録物識別子タイプ | NCID | |||||
| 収録物識別子 | AA0086707X | |||||
| ISSN | ||||||
| 収録物識別子タイプ | PISSN | |||||
| 収録物識別子 | 0549-3811 | |||||
| ISSN | ||||||
| 収録物識別子タイプ | EISSN | |||||
| 収録物識別子 | 2189-4205 | |||||
| 著作権関連情報 | ||||||
| 権利情報 | Copyright (c) 2013 The Japan Society for Aeronautical and Space Sciences | |||||
| 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 | Ablator | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Carbon Fiber Reinforced Plastic (CFRP) | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Re-entry | |||||
| 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 | 7985 | |||||
