| 可重复使用热防护系统设计要求与设计方法浅析 |
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| 引用本文： | 任青梅.可重复使用热防护系统设计要求与设计方法浅析[J].飞机设计,2014(5):44-47. |
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| 作者姓名： | 任青梅 |
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| 作者单位： | 中国飞机强度研究所全尺寸飞机结构静力、疲劳航空科技重点实验室,陕西西安710065 |
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| 摘 要： | 对高速飞行器可重复使用热防护系统的设计方法进行研究,综合分析了国外热防护系统设计思想及设计准则的发展演变,总结了国外热防护系统定尺寸分析方法,指出高超声速飞行器热防护系统设计中应考虑的关键问题,对可重复使用热防护系统的设计有一定参考意义。
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| 关 键 词： | 高速飞行器 热防护系统 设计准则 |
Overview of Design Request and Analysis Method of Reuseful Thermal Protection System |
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| REN Qing-mei.Overview of Design Request and Analysis Method of Reuseful Thermal Protection System[J].Aircraft Design,2014(5):44-47. |
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| Authors: | REN Qing-mei |
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| Institution: | REN Qing-mei ( Aircraft Strength Research Institute of China, Aeronautics Science and Technology Key Laboratory of Full Scale Aircraft Structure Static and Fatigue, Xi＇an 710065, China ) |
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| Abstract: | The design method used for hypersonic vehicle reuseful thermal protection system was researched. The development about design ideal and guide line of thermal protection system was analysed. The sizing method of thermal protection system was summarized in this paper. The key issue about design of thermal protection system for hypersonic vehicle was presented also. This paper would be reference for design of reuseful thermal protection system. |
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| Keywords: | hypersonic vehicle thermal protection system design criteria |
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