FIELD: guided rockets and missiles. SUBSTANCE: the missile has stabilizers folded onto the side surface, controls folded inside and a controls unfolding mechanism including a base. An electric primer is installed in the base, and a working chamber and a high-pressure chamber interconnected by a throttle are made. The electric primer of the controls unfolding mechanism are made with a pyrotechnical delay. Installed opposite the electric primer in the high-pressure chamber is a thin-walled cylindrical cap with clearance h from the chamber wall, positioned on which is the throttle with diameter d, condition d>h>d/4. is provided. EFFECT: enhanced accuracy of missile control. 1 dwg
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Authors
Dates
2004-02-20—Published
2002-06-19—Filed