FIELD: rocket launchers.
SUBSTANCE: invention relates to a control system for multiple rocket launchers. The block of the control system of a rocket launched from a tubular guide contains a body and aerodynamic rudders mounted on it. The rudders consist of a base, a compression-torsion spring and a shaft. L-shaped grooves are formed in the base, the bushing is fixed on the base by fixing elements in the form of diametrically located pins with the possibility of turning in the L-shaped grooves and rigid fixation by means of a locking screw. A through hole is formed in the bushing perpendicular to the longitudinal axis. A through threaded hole is made on the front end of the bushing with the possibility of installing a plug, and on the front end of the shaft there is a blind threaded hole, while the bushing is fastened to a compression-torsion spring.
EFFECT: invention is aimed at improving the manufacturability of the control system unit, providing multiple assembly (disassembly), access to the unfolding mechanism during routine maintenance without disassembling it, eliminating the use of special equipment, without deteriorating operational characteristics and reducing reliability.
1 cl, 2 dwg
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