Stability and Evolution of Orbits around Binary Asteroids: Applications to the Marco Polo Mission Scenario

Details Stability and Evolution of Orbits around Binary Asteroids: Applications to the Marco Polo Mission Scenario Stability and Evolution of Orbits around Binary Asteroids: Applications to the Marco Polo Mission Scenario

Oct 2011

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2011epsc.conf.1085w&link_type=abstract

EPSC-DPS Joint Meeting 2011, held 2-7 October 2011 in Nantes, France. http://meetings.copernicus.org/epsc-dps2011, p.1085

Physics

Scientific paper

We have analyzed the orbit stability of a spacecraft moving around a
small Near-Earth-Asteroid (NEA), focusing on the primary target of the
Marco Polo Mission: 175706 (1996 FG3). The simulation showed that most
orbits are unstable over time but under certain conditions the S/C stays
in orbit without crashing or escaping into space.

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