CONTROL UNIT OF COMPLETE FITTING OF SPIN-STABILIZED MISSILE Russian patent published in 2006 - IPC F42B15/00 

Abstract RU 2272241 C2

FIELD: armament.

SUBSTANCE: the control unit has a roll-stabilized nose module, tail module hinge-joined to it and rotating together with the acceleration unit, and missile controls. The missile controls are made in the form of impulse jet engines, which are positioned on the tail module and electrically coupled to the nose module via sliding contacts made for transmission of the control signal to the impulse jet engines for their subsequent actuation.

EFFECT: simplified construction of the missiles.

3 dwg

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RU 2 272 241 C2

Authors

Kulakov Valerij Alekseevich

Lavrenov Aleksandr Nikolaevich

Smirnov Andrej Vladimirovich

Dates

2006-03-20Published

2001-04-13Filed