GUIDED MISSILE Russian patent published in 2006 - IPC F42B15/00 

FIELD: armament.

SUBSTANCE: the guided missile has a control compartment, acceleration engine, warhead, booster engine and a tail section with a coil of the wire communication line, and the tailplane cantilevers. The acceleration engine is located between the control compartment and the warhead, whose body is made in the form of a thin-walled shell consisting of two parts. One part is made in the form of a truncated cone, whose larger base joins the other part having a permanent section. The booster engine is positioned near the smaller base, the coil of the wire communication line is wound on the engine body, the winding width of the coil does not exceed half the length of the booster engine body. The tailplane cantilevers are fastened to the booster engine body, the clearance exceeds the height of the coil winding of the wire communication line. The height of stacking of the cantilevers together with the diameter of the booster engine body does not exceed the diameter of the larger base of the truncated cone of the warhead body.

EFFECT: enhanced efficiency of the guided missile.

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