It was considered that the establishment of radiographic IQI standard for solid rocketmotorchamber was necessary.
认识到建立固体火箭发动机燃烧室X射线探伤像质计标准势在必行。
2
Two phase flow in the solid rocketmotor combustion chamber under overload condition is studied with numerical method.
对过载状态下固体火箭发动机燃烧室内二相流动进行了数值研究。
3
The ignition of the solid rocketmotor (SRM) is a very complex physical and chemistry process, which is composed of three component phases: ignition delay, flame spreading and chamber filling.