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。
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.
出处
《中国空间科学技术》
EI
CSCD
北大核心
1991年第1期17-21,6,共6页
Chinese Space Science and Technology
关键词
航天器
防热结构
局部防热
设计
Hot weather construction,Local thermal-protection,Design.
