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本文叙述了地空导弹总体性能的飞行试验结果分析方法,导弹总体性能主要包括;飞行速度、最小近界斜距、最大远界斜距、机动性。文中介绍的计算分析方法在中低空导弹的研制过程中已经应用过,并取得了满意的结果。文中的试验数据和曲线取自主翼控制布局的中低空导弹飞行试验结果,提供的分析方法和计算公式同样可以适用于其他类型的地空导弹。
This paper describes the method of flight test results for the overall performance of surface-to-air missiles. The overall performance of the missile mainly includes: flight speed, minimum near-range slant range, maximum remote slant range and mobility. The method of calculation and analysis presented in this article has been applied in the development of low-mid-range missiles and satisfactory results have been obtained. The experimental data and curves in this paper are taken from the flight test results of low-mid-to-low-altitude missiles in the control layout of the main wing. The analysis methods and calculation formulas provided are also applicable to other types of surface-to-air missiles.