背驮式空射火箭分离技术

Separation Technology of Captive-on-Top Air-Launched Vehicle

箭/机组合体的安全分离是背驮式空射系统的一项关键技术。以采用伊尔-76作为发射平台的背驮式方案为研究对象,建立箭/机分离的动力学模型,采用CFD方法计算气动力,应用特征点法进行碰撞判断,完成了分离过程的仿真计算。结果表明,火箭与载机能顺利实现分离,没有发生碰撞。

Safe separation of vehicle launched from carrier is a key technology for captive on top airlaunched system. A captive-on-top project choosing IL-76 as the carrier is studied in this paper. A dynamical mathematical model for the separation is set up. The aerodynamic force during the separation is calculated through the way of CFD method, and characteristic point method is applied to collision judgment. The results indicate that the separation of vehicle launched from the carrier can be achieved successfully and no collision occurs during the separation.