FIELD: space engineering.
SUBSTANCE: invention relates to systems for separating spacecraft (SC) and scale is used to ascent small spacecraft weighing from 1 to 50 kg into orbit. Device for SC (2) ascent contains base (3), on which SC is held by flexible conductive plates (1). Plates are connected to the power supply unit. When giving the command from the program-temporary device, base (3) is separated from plates (1), and in the plates, mutually opposite currents are excited, causing the plates to push away from each other and the appearance of a force pushing SC (2) from the carrier.
EFFECT: technical result consists in increasing the reliability of the device.
1 cl, 1 dwg
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