破障模拟弹发动机静态试验研究  

Static Experimental Study of Simulate Obstacle-Destory Rocket Engine

作　　者：徐强[1] 杨为民[1] 严世泽[1] 

机构地区：[1]南京理工大学,南京210094

出　　处：《弹箭与制导学报》1999年第3期11-14,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：介绍对破障模拟弹发动机在静止发动机试验台上进行的试验研究。模拟弹分为串联和并联两种结构形式。该项研究主要测量了发动机的推力和燃烧室压力。利用对测量结果的分析改进了模拟弹的设计。The experimental study of simulate obstacle-destory rocket engine was carried out on static experiment platform. The simulate obstacle-destory rockets were studied in two types. They were serial and parallel types. The combustion chamber pressure and propulsive force were tested. By using of the study results, the design and the flight status of simulate rocket's were improved. [

关 键 词：发动机 破障弹 模拟弹 静态试验 

分 类 号：TJ413.8[兵器科学与技术—火炮、自动武器与弹药工程]