Detailed Surface Thermal Design of the Mars 2020 Rover

dc.creatorKempenaar, Jason
dc.creatorNovak, Keith
dc.creatorRedmond, Matthew
dc.creatorFarias, Edgardo
dc.creatorSingh, Kaustabh
dc.creatorWagner, Mark
dc.date.accessioned2018-07-06T22:03:22Z
dc.date.available2018-07-06T22:03:22Z
dc.date.issued2018-07-08
dc.descriptionJason Kempenaar, Jet Propulsion Laboratory
dc.descriptionKeith Novak, Jet Propulsion Laboratory
dc.descriptionMatthew Redmond, Jet Propulsion Laboratory
dc.descriptionEdgardo Farias, Jet Propulsion Laboratory
dc.descriptionKaustabh Singh, Jet Propulsion Laboratory
dc.descriptionMark Wagner, Jet Propulsion Laboratory
dc.descriptionICES102: Thermal Control for Planetary and Small Body Surface Missions
dc.descriptionThe 48th International Conference on Environmental Systems was held in Albuquerque, New Mexico, USA on 08 July 2018 through 12 July 2018.
dc.description.abstractA new Mars rover, the Mars 2020 rover, designed by NASA’s Jet Propulsion Laboratory is scheduled to launch in July 2020. While the Mars 2020 rover is based closely on the Mars Science Laboratory rover, the design evolved to accommodate eight new science instruments and a new Sampling and Caching Subsystem (SCS) to collect samples for possible future return to Earth. Beyond the instruments and SCS, the Mars 2020 rover has several other new payloads, including additional cameras to capture Entry, Descent, and Landing (EDL). A small coaxial-rotor helicopter has also been proposed. The detailed thermal design of the Mars 2020 rover is complete. This paper describes the evolution of the thermal design from the preliminary design to the detailed design.en_US
dc.identifier.otherICES_2018_53
dc.identifier.urihttp://hdl.handle.net/2346/74064
dc.language.isoengen_US
dc.publisher48th International Conference on Environmental Systemsen_US
dc.subjectMars 2020 Rover
dc.subjectMars Rover
dc.subjectThermal Design
dc.subjectHRS
dc.titleDetailed Surface Thermal Design of the Mars 2020 Roveren_US
dc.typePresentationen_US

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