CONTROLLED BULLET IN LAUNCHING CONTAINER Russian patent published in 2015 - IPC F42B15/00 

FIELD: weapons and ammunition.

SUBSTANCE: claimed bullet comprises mid flight stage connected by wiring harness with launching container, jettisonable booster engine and adapter cowl. Detachable cams that centre controlled bullet in container are arranged between sais cowl and said container. Mid flight stage is fitted in central tube located in jettisonable booster engine. Adapter cowl houses centring grooved tube to locate said mid flight stage in axial, radial and angular directions. Wiring harness is brought outside said mid flight stage behind centring tube via adapter cowl and cam and connected with electric connector arranged at launching container. Controlled bullet incorporates wiring harness of stages coupling brought out from mid flight stage along with wiring harness. Adapter cowl centring tube features sharp edge arranged ahead of said wiring harness of stages coupling brought out from mid flight stage along with wiring harness in flight direction while said cam houses a hollow bush with internal sharp edge.

EFFECT: higher bullet efficiency.

5 dwg