烧蚀防热

返回式卫星烧蚀防热结构的工程计算

An engineering computation of ablative thermal protection structure of RETURNABLE SATELLITE

弹道式再入航天器的烧蚀防热结构设计

Ablative thermal protection structure design of return module

固体发动机有机烧蚀防热涂层的研究

Study of organic ablative thermal-protection coating for solid rocket motor

研究了二种烧蚀防热材料的显微结构。

The microstructures of two ablative materials were studied .

我国高性能烧蚀防热材料用酚醛树脂研究进展

Research on Phenolic Resin for Ablative Materials in China

酚醛纤维/酚醛复合材料烧蚀防热性能研究

Research on Ablation and Thermal Protection Properties of Phenolic Fiber / Phenolic Composites

低密度烧蚀防热透波多功能复合材料的研究

Study of multi-function composites with low density ablation heat protection and wave transmition

纳米炭黑对酚醛树脂烧蚀防热性能的影响

Effects of nanometer carbon powder on the ablative and heat-protection properties of phenolic resin

较高的温度，需要更强有力的套管和喷嘴材料，绝缘，或烧蚀防热涂料。

Higher temperatures require more robust casing and nozzle materials , insulation , or ablative coatings .

载人飞船返回舱的烧蚀防热介绍弹道式再入航天器烧蚀防热结构设计，文中说明了方案、材料选择、设计和分析计算。

ABLATIVE THERMAL PROTECTION OF CAPSULE TYPE RE-ENTRY VEHICLE This paper introduces ablative thermal protection structure design of a return module of some satellites .

介绍了在CARDC等离子体风洞中开展的非烧蚀型防热材料超高温陶瓷（UHTC）的试验研究结果。

The test results of non-ablative ultra-high temperature ceramic materials ( UHTC ) in one of the plasma wind tunnels of CARDC are introduced in this paper .