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Targeting low-energy transfers to low lunar orbit

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dc.contributor.author Parker, Jeffrey S.
dc.contributor.author Anderson, Rodney L.
dc.date.accessioned 2013-10-11T19:49:17Z
dc.date.available 2013-10-11T19:49:17Z
dc.date.issued 2011-07-31
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, July 31 ‐ August 4, 2011 en_US
dc.identifier.clearanceno 11-2820
dc.identifier.uri http://hdl.handle.net/2014/43850
dc.description.abstract A targeting scheme is presented to build trajectories from a specified Earth parking orbit to a specified low lunar orbit via a low-energy transfer and up to two maneuvers. The total transfer ΔV is characterized as a function of the Earth parking orbit inclination and the departure date for transfers to each given low lunar orbit. The transfer ΔV cost is characterized for transfers constructed to low lunar polar orbits with any longitude of ascending node and for transfers that arrive at the Moon at any given time during a month. 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, 2011. en_US
dc.subject mission designs en_US
dc.subject low energy en_US
dc.subject Earth-Moon en_US
dc.subject low lunar orbit en_US
dc.title Targeting low-energy transfers to low lunar orbit en_US
dc.type Preprint en_US


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