FIELD: astronautics.
SUBSTANCE: invention relates to the field of missile technology, namely to folding aerodynamic surfaces and mechanisms for their deployment. Opened, hinged on the body of the wing and the mechanism for opening the wing brackets, made in the form of T-shaped rotating rods installed perpendicular to each other, one of which is able to move along the axis of the other and along the wing console, and the second is pivotally attached to the other stage of the rocket. Wing is opened behind its back edge with the help of two fingers (plates) mounted on one of the levers of the opening mechanism.
EFFECT: technical result consists in providing a simpler design for the manufacture of the mechanism, the absence of its adjustment and, as a consequence, in eliminating possible errors in the assembly, as well as in reducing the mass of the rocket by reducing the number of parts.
1 cl, 6 dwg
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