| 防热结构的局部防热研究 |
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| 引用本文： | 吴国庭.防热结构的局部防热研究[J].中国空间科学技术,1991,11(1):17-21,6. |
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| 作者姓名： | 吴国庭 |
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| 作者单位： | 北京空间飞行器总体设计部 |
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| 摘 要： | 对回收式返回器的分析结果表明,表面的突起物是防热结构局部过热的重要起因。分析了防热结构的局部过热现象,提出了一种局部防热结构设计分析方法。分析计算结果与地面试验和飞行结果进行了分析比较。
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| 关 键 词： | 航天器 防热结构 局部防热 设计 |
LOCAL THERMAL-PROTECTION DESIGN PROGRAM OF RETURN MODULE |
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| Wu Guoting.LOCAL THERMAL-PROTECTION DESIGN PROGRAM OF RETURN MODULE[J].Chinese Space Science and Technology,1991,11(1):17-21,6. |
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| Authors: | Wu Guoting |
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| Institution: | Beijing Institute of Spacecraft System Engineering |
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| Abstract: | An analysis of returned overheated structure is conducted.The
results showed that outstanding objects are one of the most important causes
leading structure to local overheating.The design analysis,tests and flight
results of a local thermal-protection structure are introduced.The program is veri-
fied to be practical and reliable. |
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| Keywords: | Hot weather construction Local thermal-protection Design |
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