载人飞船返回舱的烧蚀热防护技术研究和试验表明，碳化烧蚀材料是再入飞行器最有效的热防护层。
Investigations and experiments indicate that charring ablators provide the most efficient thermal protection shield for the re-entry vehicles.
本文给出了电离空气环境中碳化材料热化学烧蚀参数的计算方法。
The method for computing the thermochemistry Ablation parameters of charred materials in ionized air environment is given in this paper.
本文给出了电离空气环境中碳化材料热化学烧蚀参数的计算方法。
The method for computing the thermochemistry Ablation parameters of charred materials in ionized air environment is given in this paper.
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