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KIAM Preprint № 190, Moscow, 2018
Authors: Baranov A.A., Grishko D.A., Ryltsova E.A., Garanin O.D., Rzaev A.F.
Flights between space debris objects in the vicinity of the geostationary orbit
Abstract:
The paper regards the problem of finding the optimal sequence of transfers between large-size space debris objects aimed at their de-orbiting from the vicinity of geostationary orbit (GEO). A flight from one object to another is carried out by a special space vehicle (SV)-collector. It is supposed that an SV approaches a debris object, captures it using a robotic arm and installs a detachable unit on its surface. Using its own propulsion system this unit ensures the object's de-orbiting to the disposal orbit which is situated above GEO region.
Keywords:
geostationary orbit, large-size space debris, space vehicle-collector, thruster de-orbiting kit, disposal orbit, GEO safety zone, inclination evolution portrait
Publication language: russian,  pages: 27
Russian source text:
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