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随着空中目标机动性的提高,近距格斗、大离轴发射时对空空导弹的性能提出了更高的要求,世界先进的空空导弹相继采用了推力矢量控制技术。本文对俄罗斯R-73空空导弹推力矢量及副翼机构工作原理及结构布局特点进行了分析。
With the improvement of maneuverability in the air targets, the requirements for air-to-air missiles are put forward higher requirements for short-range combat and large off-axis launches. The world’s advanced air-to-air missiles have successively adopted the thrust vector control technology. This paper analyzes the working principle and structural layout of the thrust vector and ailerons of Russian R-73 A / T missiles.