• DocumentCode
    445123
  • Title

    An alternative feed design for the MRO antenna

  • Author

    Imbriale, William A.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    3A
  • fYear
    2005
  • fDate
    3-8 July 2005
  • Firstpage
    761
  • Abstract
    NASA´s Mars Reconnaissance Orbiter (MRO) (see http://marsprogram.jpl.nasa.gov/mro/), scheduled for launch in 2005, is intended to study the history of water on Mars. The current feed design for the 3-meter reflector antenna uses a dielectrically supported disk-on-rod Ka-band (32 GHz) feed in the center of an X-band (7.2 GHz, 8.4 GHz) corrugated horn. As a potential backup design in case of problems, an alternate feed design for the MRO antenna that does not use any dielectric materials or a disc-on-rod was developed. The design uses a Ka-band Potter horn in the center of the current X-band MRO corrugated horn. Using the same high-gain reflector assembly, the new feed provides virtually the same X-band gain (within 0.1 db) and more than 1 dB improvement at Ka-band.
  • Keywords
    horn antennas; reflector antenna feeds; space vehicle antennas; 3 m; 32 GHz; 7.2 GHz; 8.4 GHz; Ka-band; Mars Reconnaissance Orbiter; NASA; Potter horn; X-band; corrugated horn; disk-on-rod antenna; reflector antenna feed; Antenna feeds; Apertures; Coaxial components; Frequency; Geometry; Laboratories; Mars; Propagation losses; Propulsion; Reconnaissance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Antennas and Propagation Society International Symposium, 2005 IEEE
  • Print_ISBN
    0-7803-8883-6
  • Type

    conf

  • DOI
    10.1109/APS.2005.1552367
  • Filename
    1552367