摘要
热防护系统是可重复使用航天器的核心部分,在发射或返回过程中极为重要。本文简要介绍了航天器上的主要防热部件的材料及其结构设计特点,对热防护材料进行了综合叙述,并对可重复使用航天器热防护系统进行简单介绍。
Thermal Protection System( TPS), which is the core part of the reusable astrovehicle, has been taking an important part in the process of lift-off and re-entry. This paper briefly introduces materials and structural design characters of the main thermoresistant components on the astrovehicle, it also comprehensively recounts the thermal protective materials. Further more, it simply introduces the TPS of the reusable astrovehicle.
引文
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