Journal of Projectiles, Rockets, Missiles and Guidance >
Research on Material Structure Integration Design of Missile Magnesium Alloy Components
Received date: 2013-06-13
Online published: 2025-05-26
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.
Key words： missile; magnesium alloy; integration design
ZHOU Yuhong , ZHANG Yongli , JING Tao , ZHANG Liangliang , ZHANG Yue , YAO Sheng . Research on Material Structure Integration Design of Missile Magnesium Alloy Components[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(6) : 46 -48,55 . DOI: 10.15892/j.cnki.djzdxb.2013.06.025
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