固体火箭发动机 solid rocket engine
- 分析和试验说明,固体火箭发动机在采取了合理的消除静电措施的情况下,是可以避免静电放电着火发生的。
Results of analysis and test show the accident ignition of SRM by ESD can be avoided if the proper measures of electrostatic elimination are used. - 随着底排—火箭复合增程弹的发展,对固体火箭发动机在高速旋转条件下工作性能的要求越来越高。
Technology advancements in Base-bleed and Rocket Combined Improved Range Projectile have led to demanding requirements for the working performance of solid propellant rocket engine. - 分析了固液发动机推进剂的燃烧特性和发动机性能特性、与液体和固体火箭发动机的不同,以及研制的技术难度等。
The propellant feature of burning behavior and engine in hybrid engine, the differences to liquid and solid engine and the difficulties of technology in development were analyzed.
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