FIELD: space.
SUBSTANCE: invention relates to equipment of spacecrafts (artificial satellites) and means of its deployment in orbit. Device has two identical mutually balanced in terms of weight pairs of linear guide mechanisms, installed symmetrically in vertical parallel planes. Each pair, in its turn, comprises pair of flat mirror symmetric and balanced cantilever mechanisms with common support horizontal crossbar. Top ends of outer wings are jointed with deployed spacecraft (SC) in area of its center of gravity, while bottom ends are articulated with crossbar slides. Latter are provided with drives of their synchronous movement in mutually opposite directions. Device provides movement of center of mass of SC along local vertical direction, meeting equilibrium position of satellite in circular working orbit.
EFFECT: technical result of invention consists in reduction of disturbing actions on satellite during SC deployment in orbit.
8 cl, 7 dwg
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