FIELD: transport.
SUBSTANCE: invention relates to space engineering, particularly, to devices intended for fastening payload to spacecraft. Docking device comprises receiving assembly and that to be mounted equipped with jointing surfaces, lock, guide pins and one ball stop, lead-in surface for guide pins for rough adjustment and seat for ball stop for fine adjustment. Lead-in surface represent recesses made on lateral surface of one said assemblies and inclined to axis perpendicular to surface to be jointed at acute angle with its aperture facing said surface.
EFFECT: better visual control over docking.
2 cl, 5 dwg
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