Ion Beam Shepherd for Asteroid Deflection
Space Physics
2011-02-08 v1
Abstract
We present a novel concept to impart a continuous thrust to an Earth threatening asteroid from a hovering spacecraft without need for physical attachment nor gravitational interaction with the asteroid. The concept involves an ion thruster placed at a distance of a few asteroid diameters directing a stream of quasi-neutral plasma against the asteroid surface resulting into a net transferred momentum. As the transmitted force is independent of the asteroid mass and size the method allows deflecting subkilometer asteroids with a spacecraft much lighter when compared to a gravity tractor spacecraft of equal deflection capability. The finding could make low-cost asteroid deflection missions possible in the coming years.
Cite
@article{arxiv.1102.1276,
title = {Ion Beam Shepherd for Asteroid Deflection},
author = {C. Bombardelli and J. Pelaez},
journal= {arXiv preprint arXiv:1102.1276},
year = {2011}
}
Comments
6 pages, 5 figures