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Flight path control strategies and preliminary deltaV requirements for the 2007 Mars Phoenix (PHX) mission

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dc.contributor.author Raofi, Behzad
dc.date.accessioned 2005-10-11T19:28:47Z
dc.date.available 2005-10-11T19:28:47Z
dc.date.issued 2005-08
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, CA, August 7-11, 2005 en
dc.identifier.clearanceno 05-2178
dc.identifier.uri http://hdl.handle.net/2014/37666
dc.description.abstract This paper describes the methods used to estimate the statistical deltaV requirements for the propulsive maneuvers that will deliver the spacecraft to its target landing site while satisfying planetary protection requirements. the paper presents flight path control analysis results for three different trajectories, open, middle, and close of launch period for the mission. en
dc.description.sponsorship NASA en
dc.format.extent 1008502 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. en
dc.subject Phoenix en
dc.subject deltaV en
dc.subject maneuver en
dc.subject TCM en
dc.subject Mars en
dc.title Flight path control strategies and preliminary deltaV requirements for the 2007 Mars Phoenix (PHX) mission en
dc.type Preprint en


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