GUIDED MISSILE Russian patent published in 2001 - IPC

FIELD: jet artillery ammunition. SUBSTANCE: the guided missile has a body, control equipment, timer, jet power plants, magnetoelectric generator and a thermoelectric battery for gyro starting. The electronic timer is a component of the control equipment and electrically coupled via the jet power plants to the thermoelectric battery for gyro starting. The battery ignition circuits are connected to the magneto-electric generator rigidly installed in the miscible body in parallel with its longitudinal axis, the armature of the magnetoelectric generator is made in the form of a bob-weight oriented towards the side opposite the missile flight. A cavity is formed behind the armature for its movement. The length of the armature free travel is at least 1/5 of its diameter. EFFECT: simplified design of the missile, reduced labor content of its manufacture, and enhanced reliability of use. 2 cl, 3 dwg