• DocumentCode
    2788077
  • Title

    Communications blackout predictions for atmospheric entry of Mars Science Laboratory

  • Author

    Morabito, David D. ; Edquist, Karl T.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., USA
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    489
  • Lastpage
    500
  • Abstract
    The Mars Science Laboratory (MSL) is expected to be a long-range, long-duration science laboratory rover on the Martian surface. MSL will provide a significant milestone that paves the way for future landed missions to Mars. NASA is studying options to launch MSL as early as 2009. There are three elements to the spacecraft; carrier (cruise stage), entry vehicle, and rover. The rover has a UHF proximity link as the primary path for EDL communications and may have an X-band direct-to-Earth link as a back-up. Given the importance of collecting critical event telemetry data during atmospheric entry, it is important to understand the ability of a signal link to be maintained, especially during the period near peak convective heating. The received telemetry during entry (or played back later) allows for the performance of the entry-descent-landing technologies to be assessed. These technologies include guided entry for precision landing, a new sky-crane landing system and powered descent. MSL will undergo an entry profile that may result in a potential communications blackout caused by ionized particles for short periods near peak heating. The vehicle will use UHF and possibly X-band during the entry phase. The purpose of this report is to quantify or bound the likelihood of any such blackout at UHF frequencies (401 MHz) and X-band frequencies (8.4 GHz). Two entry trajectory scenarios were evaluated: a stressful entry trajectory to quantify an upper-bound for any possible blackout period, and a nominal trajectory to quantify likelihood of blackout for such cases.
  • Keywords
    Mars; planetary rovers; space communication links; space telemetry; 401 MHz; 8.4 GHz; EDL communications; Mars Science Laboratory; Martian surface; NASA; UHF proximity link; X-band frequency; atmospheric entry; communications blackout prediction; direct-to-Earth link; entry trajectory; science laboratory rover; signal link; space vehicles; telemetry data; Atmosphere; Electrons; Frequency; Laboratories; Mars; NASA; Plasma density; Plasma temperature; Space vehicles; Telemetry;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559339
  • Filename
    1559339