FIELD: ammunition.
SUBSTANCE: invention relates to ammunition, in particular to guided missiles. The guided missile is designed to be placed in a reusable launcher equipped with transceiver antennas and launch circuits. The steering compartment is made in the form of a control module for aiming at a target using a laser-beam control channel (LBCC) or a laser guidance system (LGS), including an electric steering drive, a hydraulic coordinator that determines the roll angle, including determining the initial roll angle when installing a guided missile in a reusable launcher, an electronics unit with receiving equipment LBCC or LGS and a power supply unit. On the outer surface of the control module for targeting by LBCC or LGS, aerodynamic rudders and destabilizers with photodiodes are installed with the possibility of unfolding against the direction of flight. The electronics unit, according to the data received from the hydrocoordinator and the LBCC or LGS receiving equipment, transmits control signals to the electric steering drive.
EFFECT: rocket with unified components is being created, placed in a reusable launcher.
9 cl, 1 dwg
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Authors
Dates
2022-05-16—Published
2022-01-25—Filed