• 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