Adopting the optimization rules applied to SRM, design variables and constraints are determined from the computational model of the mass and the performance for the SRM, then the optimization model of the SRM of ASAT(anti-satellite missile) is built.

• 首先建立了固体火箭发动机的质量计算模型和性能计算模型,分析了优化指标、设计变量和约束条件,并在此基础上建立了直接上升式反卫星导弹的发动机优化数学模型。