FIELD: military equipment.
SUBSTANCE: invention relates to military equipment and, in particular, to guided missiles. Control unit includes power supply source, onboard equipment for remote reception of flight task, electric steering drive and control equipment. Control equipment comprises onboard computer, unit of inertial sensors and satellite navigation equipment. Control unit of jet projectile provides initial flight of projectile along ballistic trajectory. This unit includes wing. It has at least two cantilevers and mechanism of propulsion unit separation. Control unit is installed between warhead and propulsion unit. Equipment for remote reception of flight task is intended for reception of coordinates of target and cyclogram of operation of control unit in flight. Onboard computer is used to start execution of the cyclogram and generate control commands to the electric steering drive. During separation of propulsion system it is possible to open aerodynamic rudders and cantilevers of wing, as well as volplaning flight of projectile to target with height exceeding with subsequent defeat of target from dive.
EFFECT: enlarging combat capabilities of reactive artillery during firing at small-size targets.
4 cl, 3 dwg
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Authors
Dates
2019-12-16—Published
2019-02-25—Filed