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Analysis of various two synodic period Earth-Mars cycler trajectories

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dc.contributor.author Byrnes, D. V. en_US
dc.contributor.author McConaghy, T. T. en_US
dc.contributor.author Longuski, J. M. en_US
dc.date.accessioned 2004-09-17T07:05:28Z
dc.date.available 2004-09-17T07:05:28Z
dc.date.issued 2002-08-04 en_US
dc.identifier.citation AIAA/AAS Astrodynamics Specialist Conference en_US
dc.identifier.citation Monterey, CA, USA en_US
dc.identifier.clearanceno 02-1734 en_US
dc.identifier.uri http://hdl.handle.net/2014/9629
dc.description.abstract Trajectories that regularly encounter Earth and Mars but use small or no propulsive maneuvers are known as cycler trajectories, or cyclers. For cyclers that repeat after two Earth-Mars synodic periods, several variations are possible. A detailed investigation is presented of a simple two synodic period cycler, along with several promising variations using combinations of one year and half-year phasing orbits. Analysis is included for both the circular co-planar model and with actual Earth and Mars ephemerides. en_US
dc.format.extent 3005602 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other trajectory cycler repeat orbits en_US
dc.title Analysis of various two synodic period Earth-Mars cycler trajectories en_US


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