文中针对制导武器装备对轻型化技术的迫切需求,研究将高强镁合金材料应用于导弹的结构件上。以某导弹控制舱壳体、战斗部壳体为理论分析样机,经过数学仿真计算分析,满足了导弹用镁合金结构件的材料结构一体化设计要求,验证了该材料结构一体化设计,能够实现高强镁合金在导弹上的应用。证明高强镁合金材料在制导武器装备上工程应用的可行性。

In order to meet the urgent needs of light-weight technology for guided weaponry equipment, the high strength magnesium alloy material is applied to missile components. Taking the missile control section case and the warhead case as examples, a mathematical simulation calculation and analysis on them are conducted. The result shows that it can satisfy the integration design requirements of material structure of magnesium alloy components and can realize the application of high strength magnesium alloy in the missile. Prove that high strength magnesium alloy materials in engineering application feasibility of guided weapons and equipment.