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Mars Exploration Rover: thermal design is a system engineering activity

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dc.contributor.author Tsuyuki, Glenn T.
dc.contributor.author Avila, Arturo
dc.contributor.author Awaya, Henry I.
dc.contributor.author Krylo, Robert
dc.contributor.author Novak, Keith
dc.contributor.author Phillips, Charles
dc.date.accessioned 2005-11-11T23:48:53Z
dc.date.available 2005-11-11T23:48:53Z
dc.date.issued 2003-07
dc.identifier.citation 34th International Conference on Environmental Systems, Colorado Springs, CO, July 19-22, 2004 en
dc.identifier.clearanceno 04-1103
dc.identifier.uri http://hdl.handle.net/2014/38098
dc.description.abstract The Mars Exploration Rovers (MER), were launched in June and July of 2003, repsectively and successfully landed on Mars in early and late January of 2004, repectively. The flight system architecture implemented many successful features of the Mars Pathfinder (MPF) system: A cruise stage that transported an entry vehicle that housed the Lander, which in turn, used airbags to cushion the Rover during the landing event. en
dc.description.sponsorship NASA en
dc.format.extent 3100691 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004. en
dc.subject thermal design en
dc.subject system engineering en
dc.subject lessons learned en
dc.title Mars Exploration Rover: thermal design is a system engineering activity en
dc.type Preprint en


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