| 摘要 |
FIELD: weapons. ^ SUBSTANCE: present invention pertains to weapons and is meant for use in combat with terrorists. The missile has a case with an axially symmetric shape, inside of which there is an explosive device, control system, fuel container, supersonic gas-turbine engine, working on liquid fuel, which has a supersonic air intake, a compressor, a combustion chamber and a turbine, forming a rotor and the engine case. The fuel container is joined by a fuel line fitted with a fuel pump, to the pump actuator and the combustion chamber. At the output there are four supersonic propulsive nozzles with central cowlings inside them, made with provision for axial displacement, by using cowling actuators. The control system has an on-board computer, connected to the controller of the control system, which is connected to cowling actuators. The pump actuator is connected to the engine controller, which is connected to the on-board computer. The on-board computer is connected to a transmitter-receiver with an antenna and a global positioning system receiver, also connected to the antenna. The on-board computer is also connected to the fuse controller, connected to the explosive device. ^ EFFECT: increased missile velocity, range and target accuracy and widening of functional capabilities. ^ 4 cl, 7 dwg |
