GUIDED MISSILE Russian patent published in 2002 - IPC

FIELD: artillery rocket ammunition. SUBSTANCE: guided missile has body, steering drive in fairing with unit of control equipment on its butt connected to homing head and power supply unit which includes casing, gyroscope, communication board anchored on side of body, cable assembly and block in the form of board with contacts. Communication board and block are combined in separate assembly and interconnected by means of multicore ribbon conductors tied together in one bundle. Bundle is laid to unit of control equipment in grooves made in casing, along gyroscope, between vanes, along steering drive, in grooves in unit of control equipment placed in symmetry with reference to plane passing through longitudinal axis of missile. Block is connected to unit of control equipment on side of homing head. EFFECT: simplified design, reduced labor input to manufacture of missile, raised functional reliability of missile. 2 cl, 7 dwg