FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering, particularly, to craft docking and undocking means. Spacecraft undocking system arranged between carrier rocket mainframe comprises housing with locks, pusher and solar battery wing attachment assemblies. Every solar battery wing attachment assembly is arranged at undocking system housing, under solar battery wing, and consists of a support bracket with vertically-adjustable threaded rods secured thereat to make the thrusts. Threaded rod lower ends are secured at said support bracket while their upper ends are connected via spherical tips with pressure plates. Rubber gasket is fitted between pressure plate surface at every said adjustable thrust and bottom end surface of appropriate panel of solar battery wing.
EFFECT: decreased impact and vibratory stresses.
2 cl, 5 dwg
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