FIELD: transport.
SUBSTANCE: invention refers to space engineering and may be used for installation on carrier-rocket and for separation from it of spacecraft (SC). Device includes transition frame mounted on carrier-rocket, device separating SC and carrier-rocket, and drive. This mechanism is made in form of movable rods installed in guides rectilinearly along SC periphery. Rods are kinematically connected with each other and drive by s forming kinematic circuit containing length-adjustable links. Levers are interacting with said rods essentially by ball-ends. Rods have transverse oval orifices for mating ball-ends.
EFFECT: increase of device reliability with possible significant centering dispersion of separated articles and power characteristics of drive and decrease of SC preparation time for flight.
2 cl, 5 dwg
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