The influence of structure axial vibration on the internal ballistics of solid rocket motor was investigated. 文中研究了固体发动机结构的轴向振动对燃烧室内弹道性能的影响。
Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails. 四个向外倾斜的喷管把固体火箭发动机(SRM)的排气流分成四个相等的尾巴。
Its ignition transient process plays an important role in determining whether a solid rocket motor can work normally. 星形是固体火箭发动机(SRM)常用的装药形式,而其点火瞬时过程对发动机能否正常工作起着极为重要的作用。
Design of Solid Rocket Motor(SRM) Ignition Test System 固体火箭发动机(SRM)点火试验测试系统设计
A velocity-to-be-gained guidance law for exoatmospheric targets is proposed for an interceptor with a fuel-exhaustion-shutoff solid rocket motor. 针对拦截器使用耗尽关机固体燃料发动机的情况,设计了大气层外目标拦截的速度增益导引方法。