• DocumentCode
    2946500
  • Title

    A 6-m mesh reflector antenna for SMAP: Modeling the RF performance of a challenging Earth-orbiting instrument

  • Author

    Focardi, P. ; Brown, P. ; Rahmat-Samii, Y.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2011
  • fDate
    3-8 July 2011
  • Firstpage
    2987
  • Lastpage
    2990
  • Abstract
    A complete and accurate RF model of the SMAP observatory has been presented in this paper. Extreme care has been used in modeling all the important parts of the spacecraft to provide reliable information about the performance of the instrument under various conditions. An ongoing work of RF model refinement based on the constant development of the spacecraft and instrument is also being carried on to keep the model up to date. Field of view studies have been performed and mechanical and thermal deformations are also being considered. Since radiation pattern measurements of the actual antenna are not planned, the development of this RF model represents a very important milestone for the mission.
  • Keywords
    aerospace instrumentation; aircraft antennas; antenna radiation patterns; net structures (mechanical); reflector antennas; Earth orbiting instrument; RF performance modeling; SMAP observatory; mesh reflector antenna; size 6 m; Antenna measurements; Antenna radiation patterns; Instruments; Radio frequency; Radiometry; Space vehicles; Thermal stability; Earth Science; RF modeling; deployable antennas; mesh reflectors; reflector antennas; remote sensing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Antennas and Propagation (APSURSI), 2011 IEEE International Symposium on
  • Conference_Location
    Spokane, WA
  • ISSN
    1522-3965
  • Print_ISBN
    978-1-4244-9562-7
  • Type

    conf

  • DOI
    10.1109/APS.2011.5997157
  • Filename
    5997157