DocumentCode
2267284
Title
Mars Science Laboratory entry, descent and landing system verification and validation program
Author
Mitcheltree, Robert ; Steltzner, Adam ; Chen, Allen ; SanMartin, Miguel ; Rivellini, Tomasso
Author_Institution
Jet Propulsion Lab., Pasadena, CA
fYear
0
fDate
0-0 0
Abstract
The Mars Science Laboratory (MSL) mission will land the next generation of robotic entry, descent, and landing (EDL) systems on Mars in 2010. Relative to previous missions, the MSL EDL architecture will deliver a significantly larger mass to a significantly higher altitude while maintaining a significantly tighter delivery ellipse. MSL is pushing the limits of EDL technologies qualified previously by the Mars Viking, Mars Pathfinder, and Mars Exploration Rover missions as well as introducing new elements into the architecture. Given the difficulties of conducting a meaningful end-to-end flight test on Earth, this combination introduces numerous challenges for the EDL verification and validation program. This paper discusses how system validation challenges influenced the design of the EDL architecture and highlights how some of the remaining challenges will be addressed to assure a successful landing of this unprecedented rover on Mars
Keywords
Mars; aerospace engineering; aerospace testing; aircraft landing guidance; planetary rovers; AD 2010; Mars Exploration Rover missions; Mars Pathfinder mission; Mars Science Laboratory mission; Mars Viking mission; delivery ellipse; flight test; robotic descent systems; robotic entry systems; robotic landing systems; system validation challenges; validation program; verification program; Analytical models; Biosensors; Computational fluid dynamics; Earth; Laboratories; Logic testing; Mars; Propulsion; Robots; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2006 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-9545-X
Type
conf
DOI
10.1109/AERO.2006.1655799
Filename
1655799
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