According to the thermal shielding model of solid rocket motor, an approach of ablation heat shield design of end-burning grain with embedded wire was put forward in this paper.
根据固体火箭发动机绝热防护模型，提出了一种嵌金属丝端燃装药绝热层设计方法。
This article focuses on the mechanism of preparation of thermal shielding coatings for glass and thermal shielding materials to be chosen.
本文叙述了隔热玻璃涂料的隔热原理和隔热材料的选择。
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