The manufacture quality of solid rocket engine is ensured by the constant temperature pushing core model.
恒温插芯可以确保固体火箭发动机的制造质量，远程控制可以避免事故突发带来的人员伤亡。
The paper introduces a new method of measuring combustion time with CAT technique for solid rocket engine.
介绍一种应用CAT技术确定固体火箭发动机燃烧时间的新方法。
The ablative property 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。
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