• DocumentCode
    381639
  • Title

    Ice-embedded transceivers for Europa cryobot communications

  • Author

    Bryant, Scott

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    1
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    1
  • Abstract
    Several studies have been conducted to design robotic exploration vehicles for investigating a sub-surface water ocean within Jupiter\´s moon Europa. The current data from the Galileo spacecraft indicates a possible sub-surface ocean of undetermined depth covered by a water ice crust on the order of 10 kilometres thick. The ice crust also flexes several tens of metres every Europan day due to tidal forces. This presents several design challenges, especially for the communications link back to the science team on Earth. This paper presents the modeling and analysis for a communications system that uses transceivers embedded within the ice crust. The work was done for a design study that examined using ice-embedded transceivers to communicate between a deep ice penetration "cryobot" at the liquid water ocean and a communications package on the Europan surface. This paper focuses on the microwave properties of ice and the communications link margin analysis.
  • Keywords
    Jupiter; ice; planetary rovers; planetary satellites; space communication links; space vehicles; transceivers; Europa; Jupiter satellite; communications link margin analysis; communications system; cryobot communications link; deep ice penetration; design challenges; ice microwave properties; ice-embedded transceivers; liquid water ocean; robotic exploration vehicles; sub-surface water ocean; tidal forces; water ice crust; Geoscience; Ice thickness; Jupiter; Marine vehicles; Microwave communication; Moon; Oceans; Orbital robotics; Space vehicles; Transceivers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1036854
  • Filename
    1036854