FIELD: armament.
SUBSTANCE: the device has an assembly providing adjoining of folded aerodynamic surfaces to the flight vehicle fuselage, and an actuating locking mechanism linked with the assembly provided adjoining of folded aerodynamic surfaces to the flight vehicle fuselage with a probability of detachment. The assembly providing adjoining of folded aerodynamic surfaces to the flight vehicle fuselage consists of the first catching member positioned on the tip of the folding aerodynamic surface, and the second catching member, whose one end is linked with the first catching member, and the other - with the actuating locking mechanism and made in the form of a stopper having a body with a union and a spring-loaded rod installed in the body for axial translation and engaged with the second catching member.
EFFECT: enhanced reliability of device operation.
4 dwg
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Authors
Dates
2006-09-10—Published
2005-06-17—Filed