| 摘要 |
FIELD: armament. ^ SUBSTANCE: the autopilot unit has a body with a circular bulge on the inner surface, drive fastened to the body circular bulge, power unit including bundled conductors fastened by a clamp fastened on the power unit body, passing through a slot made in the generating line in the circular bulge of the body and terminating in a circular block fastened on the front end face of the body, and an inertial gyroscope. The inertial gyroscope is fastened on the rear end face of the power unit body. The clamp is made in the form of a shaped spring. Two slots located diametrically are additionally made in the circular bulge, the distance between the slot bottoms exceeds the outer dimension of the circular block, and their width exceeds the thickness of the circular block. The circular block is provided with a radial slot at the end. A supporting ring with an interconnection strip is fastened on the front end face of the body circular bulge. The bundled conductors are located in the radial slot of the circular block and on the front side of the supporting ring interconnection strip. ^ EFFECT: reduced length of the guided missile. ^ 3 dwg
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