• DocumentCode
    1877998
  • Title

    Mars Science Laboratory entry guidance improvements study for the Mars 2018 mission

  • Author

    García-Llama, Eduardo ; Ivanov, Mark C. ; Winski, Richard G. ; Grover, Myron R. ; Shidner, Jeremy D. ; Prakash, Ravi

  • Author_Institution
    NASA, GBTech, Inc., Houston, TX, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    11
  • Abstract
    In 2011, the Mars Science Laboratory (MSL) was launched in a mission to deliver the largest and most capable rover to date to the surface of Mars. A follow on MSL-derived mission, referred to as Mars 2018, is being proposed to launch in 2018. Mars 2018 is investigating performance enhancements of the Entry, Descent and Landing (EDL) system over that of its predecessor MSL mission of 2011. This paper will discuss the main elements of the proposed Mars 2018 EDL preliminary design that are being considered to increase performance on the entry phase of the mission. In particular, these elements are discussed with the goals of increasing the parachute deploy altitude to allow for more time margin during the subsequent descent and landing phases, increasing the entry mass, and reducing the delivery ellipse size at parachute deploy, through modifications in the entry reference trajectory design, vehicle´s lift to drag ratio, parachute deploy trigger logic design, and the effect of additional navigation hardware.
  • Keywords
    Mars; navigation; planetary rovers; planetary surfaces; space vehicles; EDL preliminary design; Mars 2018 mission; Mars science laboratory entry guidance improvements study; entry reference trajectory design; navigation hardware; parachute deploy altitude; parachute deploy trigger logic design; predecessor MSL mission; time margin; Acceleration; Equations; Mars; Mathematical model; Navigation; Trajectory; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6186997
  • Filename
    6186997