FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and can be used for jointed head part to carrier rocket in vertical position. Proposed structure comprises frame with posts and supports for parts to be jointed together. Height-adjusted supports are mounted on one ends of bell cranks pivoted to posts to swing therein vertically. Opposite ends of said bell cranks resting on the frame accommodated flexible elements arranged thereon to interact with swinging levers arranged under bell cranks. Central parts of swinging levers are linked with the frame by turnbuckles designed to pre-clamp said flexible elements.
EFFECT: simplified docking and ruling out damaged carrier rocket components.
2 dwg
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