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Deflection missions for asteroid 2011 AG5

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dc.contributor.advisor Astronomy en_US
dc.contributor.author Grebow, Daniel
dc.contributor.author Landau, Damon
dc.contributor.author Bhaskaran, Shyam
dc.contributor.author Chodas, Paul
dc.contributor.author Chesley, Steven
dc.contributor.author Yeomans, Don
dc.contributor.author Petropoulos, Anastassios
dc.contributor.author Sims, Jon
dc.date.accessioned 2013-04-23T18:01:14Z
dc.date.available 2013-04-23T18:01:14Z
dc.date.issued 2012-10-29
dc.identifier.citation 23rd International Symposium on Space Flight Dynamics, Pasadena, California, October 29 - November 2, 2012, en_US
dc.identifier.clearanceno 12-5334
dc.identifier.uri http://hdl.handle.net/2014/43033
dc.description.abstract The recently discovered asteroid 2011 AG5 currently has a 1-in-500 chance of impacting Earth in 2040. In this paper, we discuss the potential of future observations of the asteroid and their effects on the asteroid’s orbital uncertainty. Various kinetic impactor mission scenarios, relying on both conventional chemical as well as solar-electric propulsion, are presented for deflecting the course of the asteroid safely away from Earth. The times for the missions range from pre-keyhole passage (pre-2023), and up to five years prior to the 2040 Earth close approach. We also include a brief discussion on terminal guidance, and contingency options for mission planning. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012. en_US
dc.subject near-Earth object en_US
dc.subject small body en_US
dc.subject impact trajectory en_US
dc.title Deflection missions for asteroid 2011 AG5 en_US
dc.type Preprint en_US


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