Tether assisted near earth object diversion
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Abstract Potential earth impact threats posed by asteroids have motivated researchers to find effective NEO diversion techniques. Several means to perturb the motion of an asteroid have been discussed in the literature. Attaching a long tether and ballast mass to the asteroid can effectively alter its trajectory. In this paper it is shown that by cutting the tether at an appropriate time the diversion can be enhanced. The instant of cutting the tether significantly affects the final orbit of the asteroid and thus the resulting deflection from the original path.
[1] T. Ahrens,et al. Deflection and fragmentation of near-Earth asteroids , 1992, Nature.
[2] Colin R. McInnes,et al. Near Earth Object Orbit Modification Using Gravitational Coupling , 2007 .
[3] Andre P. Mazzoleni,et al. Asteroid Diversion Using Long Tether and Ballast , 2009 .
[4] H. J. Melosh,et al. Solar asteroid diversion , 1993, Nature.
[5] Stanley G. Love,et al. Gravitational tractor for towing asteroids , 2005, Nature.