FIELD: astronautics.
SUBSTANCE: invention relates to the space equipment. Spacecraft-evacuator includes housing, control and power supply system devices, propulsion unit, electromechanical system of spacecraft capture in orbit. On the housing there are at least two optical chambers, a range finder, an unfolding bar, a drum with a cable fixed on the drum with possibility of movement along the rod. Free end of the cable is equipped with a detachable device for gripping in orbit of the spacecraft in the form of a latch or manipulator. Drum is made with possibility of reversible rotation, rope is made in the form of a set of power, energy and information cables. Grip device is fixed on the rod by electromechanical lock and made as controlled by cable.
EFFECT: creation of spacecraft-evacuation device of spent satellites of simplified design, which enables to carry out operations of capture of large space objects.
1 cl, 6 dwg
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Authors
Dates
2019-04-29—Published
2018-02-13—Filed