• DocumentCode
    2906343
  • Title

    Mars Reconnaissance Orbiter: extended dual-purpose mission

  • Author

    Johnston, M. Daniel Dan ; Herman, David E. ; Zurek, Richard W. ; Edwards, Charles D.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    16
  • Abstract
    The Mars Reconnaissance Orbiter (MRO) was launched from Cape Canaveral Air Force Station, Florida, aboard an Atlas V-401 launch vehicle on August 12, 2005 and entered Mars orbit on March 10, 2006. After five months of aerobraking, a series of propulsive maneuvers were used to establish the desired low-altitude science orbit. The spacecraft has been on station in its 255 × 320 km, 3 p.m., primary science orbit since September 2006 performing its scientific and UHF-relay functions. This paper provides a brief status of the prime mission and describes the plans and preparations in work for its recently approved two-year mission extension.
  • Keywords
    Mars; aerospace instrumentation; planetary surfaces; space vehicles; Atlas V-401 launch vehicle; Cape Canaveral Air Force Station; Florida; Mars Reconnaissance Orbiter; UHF-relay functions; aerobraking; extended dual-purpose mission; low-altitude science orbit; propulsive maneuvers; Instruments; Mars; Orbits; Pixel; Reconnaissance; Space vehicles; Spatial resolution;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747277
  • Filename
    5747277