GUIDED MISSILE Russian patent published in 2004 - IPC

FIELD: rocketry, applicable in small-sized missiles.

SUBSTANCE: the block of the control equipment is made of two modules, one of which contains the control actuator of the control equipment, and the other - the transceiver unit of the control equipment. The control actuator module is fastened in the front part of the body, the transceiver unit module is fastened in its rear part, and the warhead is positioned between the mentioned modules. The control actuator module and the transceiver unit module are electrically interconnected by bundled conductors passing through the warhead. The bundled conductors between the warhead and the transceiver unit module are provided with a compensator of longitudinal motions.

EFFECT: enhanced speed of missile flight in dense atmosphere layers.

2 cl, 1 dwg