摘要
总结了国内外在精确制导子弹药及自主导引头方面所做的工作,然后,根据国内的情况提出了用于封锁机场的战略导弹末制导子导弹总体方案设想,最后,论述了子导弹气动设计方面应考虑的一些技术措施,并初步估算了子导弹控制飞行所需要的过载。
The work in terms of percision guided submissiles and homing heads is Summarized. Then, according to our practical situatuns, alternatives for the terminal guided submissiles of strategic missiles attacking runway are presented. Finally, some techniques are discussed concerning submissiles' aerodynamic design, and the required overload needed in controlled flight is estimated.
出处
《战术导弹技术》
1998年第2期17-24,共8页
Tactical Missile Technology
关键词
战略导弹
精确制导
末制导
子母弹
Strategic missiles Precision guidance Terminal guidance Submunition
