整体式固冲发动机与导弹一体化优化设计

概述了发动机与导弹一体化优化设计问题，建立了整体式固部发动机与导弹一体化优化设计模型，并以某防空导弹为一算例，进行了优化前后两种方案对比，结果表明，经地定体化优化设计挖掘了整整体式固部贩设计潜力，导弹弹道性能明显提高。

The Integrated Design Optimization of Solid Rocket Ramjet and Missile

The integrated design optimization of solid rocket ramjet and missile is briefly described. Themodel for the integrated design optimization of the integral solid rocket ramjet and missile has been developed. Some air defense missile is taken for an algorithm example to compare the two concepts before and afteroptimization. It has been shown that the integrated design optimization has the great petential to be tappedfor the integral solid rocket ramjet design so as to significantly improve the ballistic performance of the thesile.