CONTROLLED BULLET Russian patent published in 2014 - IPC F42B10/12 F42B15/01

Abstract RU 2512047 C1

FIELD: weapons and ammunition.

SUBSTANCE: controlled bullet is made by two-stage double-calibre scheme and includes warhead, launch engine, control unit and gas-dynamic control device. It features transit fairing with gas-dynamic control device positioned around the tail part of sustainer stage and made in the form of gas-dynamic steering gear with toroidal gunpowder pressure tank implementing torque control by creating lateral pull. Nozzles of gas-dynamic device are brought outside of the transit fairing in radial direction. Launch engine is removable. Launch engine case is conical. Warhead is located in the head part of sustainer stage. Control unit is located in the tail part of sustainer stage inserted into central tube in the launch engine.

EFFECT: reduced weight and increased manoeuvrability of aircraft.

2 dwg

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RU 2 512 047 C1

Authors

Shipunov Arkadij Georgievich

Dates

2014-04-10—Published

2012-11-29—Filed