The test set of the Explosively Formed Projectile (EFP) with star shaped tail was designed with a multi-point initiation.
采用多点起爆方式,设计了带尾翼翻转型爆炸成形弹丸(efp)试验装置。
2
Trajectory deflection correction by miniature pulse thruster groups is an efficiency method of improving rocket projectile firing precision and reducing the scattering of impact point.
采用小型脉冲推力器组修正弹道偏差是提高火箭弹射击精度,减小落点散布的有效方法。
3
From the point of launch dynamics, the factors influencing the vertical target dispersion of projectile were analyzed.