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Mars Reconnaissance Orbiter navigation strategy for dual support of insight and ExoMars entry, descent and landing demonstrator module in 2016

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dc.contributor.author Wagner, Sean V.
dc.contributor.author Menon, Premkumar R.
dc.contributor.author Chung, Min-Kun J.
dc.contributor.author Williams, Jessica L.
dc.date.accessioned 2017-08-08T21:36:05Z
dc.date.available 2017-08-08T21:36:05Z
dc.date.issued 2015-08-09
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference, Vail, Colorado, August 9-13, 2015 en_US
dc.identifier.clearanceno 15-3089
dc.identifier.uri http://hdl.handle.net/2014/45852
dc.description.abstract This paper describes MRO Navigation's maneuver strategy to move MRO's ascending node to meet the InSight EDL phasing requirement and support EDM. 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, 2015 en_US
dc.subject MRO en_US
dc.subject maneuver en_US
dc.subject design en_US
dc.subject InSight en_US
dc.subject EDM en_US
dc.subject EDL en_US
dc.subject phasing en_US
dc.title Mars Reconnaissance Orbiter navigation strategy for dual support of insight and ExoMars entry, descent and landing demonstrator module in 2016 en_US
dc.type Presentation en_US


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