The ablativeproperty requirements and the studies on the insulation layer of solid rocket engine in oxidizer rich environment were presented.
介绍了富氧环境下固体火箭发动机对绝热层性能的要求，以及在该特殊条件下对绝热层所开展的研究工作。
2
The results also indicate, the ablativeproperty of the Mo-phenolic resin composites at high temperature is superior, and is especially outstanding under the condition of high heat flux.
同时表明，钼酚醛复合材料的高温烧蚀性能良好，特别是在高热通量条件下，性能更佳。
3
It is indicated that the sub default has influence on materials microstructure and some properties on the basis of NDT, TEM and analysis of ablative and mechanical property.