MISSILES AND GUIDANCE TECHNOLOGY

Security Release Analysis of the Missile Tail Hook on Launcher

  • SHU Tao
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2012-01-02

  Online published: 2025-05-29

Abstract

The security release analysis involving body interfere and hook retardarce is one of the most important key to air-to-air missile design. Firstly, the method was introduced, and then the influence points were given. Finally, as an example, a missile was analyzed with the method. The article provides reference for the security release analysis.

Cite this article

SHU Tao . Security Release Analysis of the Missile Tail Hook on Launcher[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(5) : 33 -35,44 . DOI: 10.15892/j.cnki.djzdxb.2012.05.025

References

[1]
郑志伟. 空空导弹系统概论[M]. 北京: 兵器工业出版社, 1997.
[2]
李新国, 方群. 有翼导弹飞行动力学[M]. 西安: 西北工业大学出版社, 2005.
[3]
陈升, 杨庆贺. 导弹发射安全技术研究[J]. 航空兵器, 2002 (5): 17- 19.
[4]
张胜利, 倪冬冬. 机载导弹武器系统导轨式发射的安全性设计. 航空兵器, 2004 (6): 24- 27.
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