Finite element analysis based on ansys of ball - socket nozzle ' s pendulous socket in solid - rocket engine 的固体火箭发动机珠承喷管摆动接头的有限元分析
Study on hybrid orbit self - adaptive guidance scheme of solid rocket motor based on depleted shutdown 基于固体火箭发动机耗尽关机的混合轨道自适应制导方案研究
Gap design of solid rocket motor nozzle was analysized through thermal and structure analysis 摘要通过热和结构计算，对固体火箭发动机喷管缝隙设计进行了分析。
A . ciucci , et al . numerical analysis of ignition transients in solid rocket motors 余贞勇，固体火箭发动机翼槽内火焰传播机理研究，西北工业大学博士论文， 2000 . 3 。
Progress and prospect in technology of monitoring and testing for health and failure determination in solid rocket motor 固体火箭发动机状态监测和失效判定技术的发展和展望
Coupling computation on radial vibration of chamber structure and internal ballistic property for solid rocket motor 固体火箭发动机燃烧室结构径向振动与内弹道性能的耦合计算
T crowe , et al . effect of spin on the internal ballistics of a solid - propellant motor r . aiaa 66 523 曹泰岳，常显奇，等.固体火箭发动机燃烧过程理论基础m .长沙：国防科技大学出版社
C t crowe , et al . effect of spin on the internal ballistics of a solid - propellant motor r . aiaa 66 523 曹泰岳，常显奇，等.固体火箭发动机燃烧过程理论基础m .长沙：国防科技大学出版社
Calculating examples are given to illustrate the application of the method on structure integral analysis of solid rocker motor 结合算例说明了该方法在固体火箭发动机结构完整性分析中的适用性。
So it has important value both on theory and practical application to perform uncertain structural analysis for srm grain 因此，进行固体火箭发动机药柱的不确定结构分析具有重要的理论价值和工程实际意义。
