COMBINED MISSILE Russian patent published in 2009 - IPC F42B15/00 

Abstract RU 2348895 C2

FIELD: weapons.

SUBSTANCE: present invention pertains to weapons and is meant for use in combat with terrorists. The combined missile has a case with axially symmetrical shape with four stabilisers. Inside the case there is an explosive device, a fuel tank, solid fuel jet engines, fitted in the rear part of the missile on its periphery. Along the axis of the missile there is a gas-turbine engine, working on liquid fuel and with an air intake, compressor, combustion chamber and a turbine. The fuel tank is anchor ring shaped and is joined by a fuel line, fitted with a fuel pump, to the combustion chamber.

EFFECT: increase in missile velocity, range and target accuracy and widening of functional capabilities of the missile.

6 cl, 4 dwg

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RU 2 348 895 C2

Authors

Bolotin Nikolaj Borisovich

Dates

2009-03-10Published

2007-05-03Filed