• DocumentCode
    1881007
  • Title

    MAVEN relay operations concept

  • Author

    Chamberlain, Neil ; Gladden, Roy ; Bruvold, Kris

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    11
  • Abstract
    The Mars Atmosphere and Volatile EvolutioN (MAVEN) mission will launch in late 2013 and, following a 10 month cruise to Mars, will study the upper atmosphere of the planet. In addition to the science instruments, the MAVEN spacecraft is equipped with an Electra UHF transceiver to support relay communication with landed assets. This paper describes how UHF relay service is provisioned by MAVEN. The discussion includes a description of the Electra payload, the process by which relay activities are coordinated and accounted for, the process of a typical relay session, including uplink and downlink, as well as special commands to calibrate and verify relay performance. The operational processes for providing these services are inherited largely from prior Mars missions and take advantage of existing infrastructure and lessons learned from those missions. Preliminary data volume return capabilities using adaptive data rates and low-density parity check channel coding are presented.
  • Keywords
    Mars; channel coding; parity check codes; radio transceivers; space communication links; Electra payload; MAVEN relay operations; MAVEN spacecraft; Mars atmosphere and volatile evolution mission; UHF relay service; adaptive data rates; electra UHF transceiver; low density parity check channel coding; operational process; relay communication; science instruments; Antenna measurements; Atmosphere; Atmospheric measurements; Mars; Relays; Space vehicles; UHF antennas;
  • 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.2012.6187114
  • Filename
    6187114