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减小尾翼式火箭散布的新途径——同是采用尾翼延迟张开和减速旋转
A New Way to Reduce Dispersion for Fin Rocket——by Using Unfolding Fins and Retarded Spin Regrurity at Same Time
【摘要】 本文在同时考虑减速旋转和尾延迟张开情况下,对火箭弹散布进行了详细的计算,并用优化设计方法找到了其最优点.为大幅度提高火箭密集度提供了一条新路.
【Abstract】 A detail clculation of dispersion has been given in this paper when using unfoldingfins and restarted spin regrurity at same time.And find the optimum point by using optimiza-tion.We obtain a new method for reducing dispersion.
- 【文献出处】 弹道学报 ,Journal of Ballistics , 编辑部邮箱 ,1992年04期
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