FIELD: space equipment.
SUBSTANCE: invention relates to space engineering, particularly, to spacecrafts and their parts docking and decoupling systems. Device for docking spacecrafts for two-stage docking process consists of extended docking assembly. Docking assembly represents structure with fixing elements on outer side. It is made with possibility of extension from carrier device by means of controlled pneumatic elements. Elements consist of a corrugated sleeve with a cable rope passing inside. Cable-rope is fixed by one end on the pneumatic element base on the docking assembly, and by another one on the servo drive in the pneumatic element body adjusting its length.
EFFECT: enabling higher reliability.
4 cl, 3 dwg
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