• DocumentCode
    3206562
  • Title

    MSL V&V CEDL Mechanical Systems test program

  • Author

    Eremenko, Alexander ; Hoffman, Pamela ; Rivellini, Tommaso

  • Author_Institution
    Jet Propulsion Lab., NASA, Pasadena, CA
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    Mars Science Laboratory is a scientific mission with exploration rover. In order to accomplish this mission, the rover must be transported from Earth to the Martian surface, including cruise, entry, descent, and landing phases (CEDL). The key challenges for testing CEDL mechanical system lie in the physical size of the spacecraft and major subassemblies, complex configuration, multiple load cases, numerous separation events, new unique ldquosky cranerdquo landing method, budget and schedule limitations, and difficulties associated with testing in Earth environments. This paper will describe the verification and validation (V&V) CEDL mechanical systems test program and key challenges of each of subsystem testsrdquo.
  • Keywords
    Mars; aerospace engineering; aerospace testing; mechanical testing; space vehicles; Martian surface; mechanical systems test program; rover; scientific mission; spacecraft; Cranes; Earth; Laboratories; Mechanical systems; NASA; Propulsion; Safety; Space vehicles; System testing; Vibrations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839588
  • Filename
    4839588