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Please use this identifier to cite or link to this item:
http://hdl.handle.net/2014/38098
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| Title: | Mars Exploration Rover: thermal design is a system engineering activity |
| Authors: | Tsuyuki, Glenn T.
Avila, Arturo
Awaya, Henry I.
Krylo, Robert
Novak, Keith
Phillips, Charles |
| Keywords: | thermal design
system engineering
lessons learned |
| Issue Date: | Jul-2003 |
| Publisher: | Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004. |
| Citation: | 34th International Conference on Environmental Systems, Colorado Springs, CO, July 19-22, 2004 |
| 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. |
| URI: | http://hdl.handle.net/2014/38098 |
| Appears in Collections: | JPL TRS 1992+
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