• DocumentCode
    3515360
  • Title

    Guide Rails for Linear Separation of Powered Descent Vehicle from Mars Science Laboratory Backshell

  • Author

    Quicksall, J.J. ; Gallon, J.C.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    During descent through the Martian atmosphere, Mars science laboratory (MSL) uses three sets of guide rails and rollers to control the separation dynamics of the powered descent vehicle (PDV) from the Backshell and parachute. The guided linear separation of the two bodies over a distance of half a meter mitigates the risk of re- contact which could result in unexpected and detrimental vehicle dynamics. The guide rails are comprised of three thin beams oriented in 120 degree intervals around the circumference of the Backshell´s internal structure, and they interface with three sets of four rollers mounted on the exterior of the PDV. This configuration resists motion in 5 DOF. The only unconstrained DOF is in the direction of desired separation. Analysis was used to size the guide rail and rollers, and tests will be performed to validate the design´s capability to perform as required during the dynamic separation event.
  • Keywords
    aerospace components; rails; space vehicles; Mars science laboratory backshell; Martian atmosphere; guide rails; linear separation; parachute; powered descent vehicle; rollers; vehicle dynamics; Atmosphere; Laboratories; Mars; Performance evaluation; Rails; Resists; Space vehicles; Vehicle driving; Vehicle dynamics; Wrist;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526534
  • Filename
    4526534