English

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

R2 v1 2026-06-21T17:22:34.795Z