MECHANISM FOR COMBINATION CONTROL OF ROCKET Russian patent published in 2008 - IPC F42B15/00 

FIELD: armament, in particular, rocket control systems.

SUBSTANCE: the mechanism for combination control of rocket has a controls system consisting of aerodynamic control surfaces and a gas dynamic control unit with four spoilers. The spoilers are kinematically linked with the aerodynamic control surfaces by means of a driving gear, which includes a carrier, shell with an inclined closed groove engageable with a ball. The toothed gear wheel on the external side of the shell gets engaged with a pinion installed on the axle of the servo actuator, and an inclined open cylindrical groove is located on the end surface of the carrier, the spherical end of the lever is positioned in this cylindrical groove.

EFFECT: provided invariance of cophased combination control of rocket from the aerodynamic and gas dynamic control surfaces simultaneously in response to a single command.

2 cl, 4 dwg