FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to deployable orbital systems. Deployable orbital system consists of spacecraft (1) and satellite (2). Both are equipped with docking devices. Spaceship and satellite have superconducting coils (5) and (10), which are supplied with currents. Superconducting switches (7) and (12) are closed to form superconducting circuits. As a result of interaction of oppositely directed currents in superconducting coils (5) and (10) there appears a repulsion force and spaceship (1) and satellite (2) move away from each other at distance x0. In superconducting coils (5) and (10) there can appear additional currents, interaction of which leads to attraction force between superconducting coils (5) and (10), and spaceship (1) and satellite (2) are attracted to preserve distance x0.
EFFECT: provided is higher system reliability.
1 cl, 1 dwg
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