SELF-POSITION ROCKET MISSILE Russian patent published in 2009 - IPC F42B15/00 

FIELD: weaponry.

SUBSTANCE: invention refers to warlike equipment and aims at embattling and antiterrorist actions. The self-position rocket missile includes the axial-symmetric case with mounted explosive assembly and fuel tank, while its back part including jet nozzle. In front of the jet nozzle there is gas-turbine engine containing the air inlet, compressor, combustion chamber and turbine. The fuel tank is attached through the fuel pipe with there mounted fuel pump to the combustion chamber. The pump drive is connected to the engine controller by-turn connected to the onboard computer. The antenna transceiver and antenna Global Position System receiver are connected to the onboard computer. The detonator controller connected to the onboard computer is by-turn connected to the explosive assembly.

EFFECT: higher target accuracy and missile enhancement.

4 cl, 5 dwg