FIELD: cosmonautics.
SUBSTANCE: device for deployment of multi-section structures contains a frame and sections with supporting elements connected by hinges equipped with drives. There are clamps, each made in the form of a spring-loaded lever. One of the arms of the lever represents a grip, and the other arm is made in the form of a support platform. The lever spring is connected to the support element of the section located first from the frame at one end, and to the lever at the other end. The frame is made with a stop. The supporting elements of the sections contain axles. The axle of the middle section is used to engage the grip. A lever is fixed on the axle of the support element of the first section from the frame. The frame contains the second stop. The stops are located in such a way that, in the folded position of the sections, the support platform of the lever rests against the first stop and moves from the first stop to the second one during deployment.
EFFECT: increased reliability of fastening.
1 cl, 6 dwg
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