FIELD: weapons.
SUBSTANCE: invention relates to weapons and can be used in small-size rocket systems. Controlled bullet comprises armour-piercing rod, stabilizing elements, aerodynamic rudders, drive unit for control elements, photoreceiver arranged in rear end of controlled bullet, on-board equipment, on-board power supply and detachable starter motor. Control unit of control elements with aerodynamic rudders is arranged in front of armour-piercing rod in direction of flight. In the armour-piercing rod the slot is made, in which the electric cable is installed. Stabilizing elements are made in the form of four cantilevers located in the plane passing through the longitudinal axis of the controlled bullet. In the lower part of the sustainer stage there is a mechanical roll gyroscope.
EFFECT: technical result consists in improvement of dynamic properties of controlled bullets and increase in accuracy of firing.
3 cl, 6 dwg
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Authors
Dates
2020-02-07—Published
2019-02-14—Filed