GUIDED MISSILE Russian patent published in 2001 - IPC

FIELD: jet artillery ammunition. SUBSTANCE: the guided missile has a body, electric power unit in the form of a yoke with sleeves accommodating a gyro and thermoelectric batteries. A clamp made in the form of a flat ring with lugs bent inside the seats for the thermoelectric batteries is rigidly attached to the end of the yoke of the electric power unit, on the side of the missile nose cone. The ends of the lugs have the shape of washers aligned with the batteries, they are provided with rubber round-shaped gaskets located with compression between the lugs and batteries. The clamp is installed in a groove made on the end of the yoke equal in diameter to the outside diameter of the clamp ring section, and envelops with its inside diameter the seat for the gyro. EFFECT: enhanced reliability of missile functioning at temperatures up to +60C. 3 dwg