On the Possible Utilization of an End-Effector Mechanism for Space Debris Remediation in Low Earth Orbit

Author:

Dawood AamirORCID,Sarosh AliORCID,Talha MuhammadORCID,Khan Wajih AhmedORCID

Publisher

Springer Nature Singapore

Reference34 articles.

1. Liou, J.-C., An active debris removal parametric study for LEO environment remediation. Advances in space research, 2011. 47(11): p. 1865-1876.

2. Kessler, D.J. and B.G. Cour‐Palais, Collision frequency of artificial satellites: The creation of a debris belt. Journal of Geophysical Research: Space Physics, 1978. 83(A6): p. 2637-2646.

3. Office, E.s.S.D. Space debris by the numbers. 2023 27 March 2023 [cited 2023 21 April 2023]; 5.0:[Available from: https://sdup.esoc.esa.int/discosweb/statistics/.

4. Murdoch, N., et al. Electrostatic tractor for near earth object deflection. in 59th International Astronautical Congress. 2008.

5. Lu, E.T. and S.G. Love, Gravitational tractor for towing asteroids. Nature, 2005. 438(7065): p. 177-178.

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