FIELD: transport.
SUBSTANCE: invention relates to space engineering, primarily to space cable systems. Proposed method comprises undocking of two objects connected by cable, imparting to the lander of initial velocity of departure, unobstructed release of cable on departure of the lander, fixation of cable length at the end of reverse section, paired pendulum motion and cutting of the cable at the moment whereat lander passes by the line of orbital station local vertical. Separation of the lander is performed against orbital velocity vector with control over cable tension force control at departure of the lander. Free cable is hauled in at trajectory reverse section.
EFFECT: implemented and efficient deployment.
4 dwg
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