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Geomagnetic Energy Approach to Space Debris Deorbiting in a Low Earth Orbit
2019
International Journal of Aerospace Engineering
The space debris removal problem needs to be solved urgently. Over 70% of debris is distributed between the 500 km and 1000 km low Earth orbits (LEO), and existing methods may be theoretically feasible but are not the high-efficiency and low-consumption methods for LEO debris removal. Based on the torque effect of a static magnet interacting with the geomagnetic field, a new spin angular momentum exchange (SAME) method by geomagnetic excitation (without working medium consumption) for LEO
doi:10.1155/2019/5876861
fatcat:frhf3yi2sjatpkvufeplr2gw5y