• DocumentCode
    3206504
  • Title

    Tension-only, moment-free, separation mechanism for Mars Science Laboratory aeroshell

  • Author

    Buecher, David ; Hund, Richard

  • Author_Institution
    Lockheed Martin Space Syst. Co., Littleton, CO
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    Lockheed Martin Space Systems Company is involved in the design and manufacture of the aeroshell for the Mars Science Laboratory (MSL) rover, an upcoming NASA-JPL mission to Mars. During entry into the Martian atmosphere, the aeroshell primarily protects the rover, as the spacecraft passes through extreme heating and dynamic pressure environments. After entering the atmosphere, and decelerating, the nine separation mechanisms, located at the Backshell to Heatshield interface, separate the aeroshell at the seam between the Heatshield (the lee-side, or entry half, of the aeroshell) and the Backshell (the aft-side of the aeroshell), to enable the successful deployment of the lander.
  • Keywords
    aerospace engineering; aerospace industry; bending; compressive strength; design engineering; planetary rovers; Heatshield entry loads; Heatshield separation hardware; Lockheed Martin Space Systems Company; Mars Science Laboratory Aeroshell; Mars Science Laboratory rover; Martian atmosphere; NASA-JPL mission; backshell ring; bending loads; compressive force; compressive loads; moment-free separation mechanism; parachute inflation; separation fittings; shear loads; tension loads; tension-only separation mechanism; Aerodynamics; Atmosphere; Fitting; Laboratories; Manufacturing; Mars; Performance evaluation; Protection; Testing; Vehicles;
  • 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.2009.4839585
  • Filename
    4839585