FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, and more specifically to spacecrafts, which can be used to combat space debris. Proposed system comprises spacecraft, solar charger and deployment system interconnected by assembly operations. Solar concentrator includes one or more optically conjugated mirrors which focus solar radiation at one point of the required diameter and connected to the deployment system. Spacecraft includes an autonomous control system, data transmission system, spacecraft stabilization and orientation system. Spacecraft accumulates solar energy and heat from solar concentrator for power supply of spacecraft.
EFFECT: elimination of small-size debris of space garbage in orbit.
1 cl, 2 dwg
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