• DocumentCode
    1878038
  • Title

    Entry, Descent, and Landing performance trades to increase landed mass for the Mars 2018 mission

  • Author

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

  • Author_Institution
    Binera, Inc., Yorktown, VA, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    13
  • Abstract
    The proposed Mars 2018 mission is a joint mission with the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA) that is currently in the early study phase. The objective would be to land a rover which caches a sample of Martian soil for retrieval and potential return to Earth on a subsequent mission. The Mars 2018 Entry, Descent, and Landing (EDL) system would largely leverage off of heritage from the Mars Science Laboratory (MSL) EDL system in an effort to minimize cost and schedule risk. Despite the desire to have high MSL heritage, a series of trade studies were performed to quantify the impact that incorporating EDL technologies would have on the landed mass. These new technologies include a trim tab, an increased diameter disk-gap-band (DGB) parachute over MSL, a large ringsail parachute, and a supersonic inflatable aerodynamic decelerator (SIAD).
  • Keywords
    Mars; aerodynamics; aerospace instrumentation; parachutes; planetary rovers; DGB parachute; EDL system; ESA; Earth; European Space Agency; Mars 2018 mission; Mars Science Laboratory; Martian soil; NASA; National Aeronautics and Space Administration; descent performance; disk-gap-band parachute; entry performance; landed mass; landing performance; ringsail parachute; rover landing; supersonic inflatable aerodynamic decelerator; Aerodynamics; Analytical models; Atmospheric modeling; Mars; Mathematical model; NASA; 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.2012.6186998
  • Filename
    6186998