• DocumentCode
    2627648
  • Title

    Definition the location of the fixing points of the reflector of the space vehicle antenna

  • Author

    Berdnikova, N.A.

  • Author_Institution
    Siberian State Aerosp. Univ., Krasnoyarsk, Russia
  • fYear
    2013
  • fDate
    12-13 Sept. 2013
  • Firstpage
    1
  • Lastpage
    3
  • Abstract
    At present should be noted that the market of space communication services is rapidly growing. The space communication are fast-developing sector of telecommunications, and represent a high interest for the investors. This caused by that large area antenna systems provide direct access the consumer to resource of spacecraft and the land operators can be omitted. In work will be considered an antenna consists of the offset reflector with size 2,5 ×4 (m) and the irradiating system in the form of a conical horn.
  • Keywords
    antenna radiation patterns; conical antennas; reflector antennas; space communication links; space vehicle antennas; antenna systems; conical horn; irradiating system; offset reflector; space communication services; space vehicle antenna; spacecraft; Educational institutions; Finite element analysis; Fluctuations; Modal analysis; Reflector antennas; Space vehicles; an offset reflector; the fixing points; the frequency of fluctuations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Communications (SIBCON), 2013 International Siberian Conference on
  • Conference_Location
    Krasnoyarsk
  • Print_ISBN
    978-1-4799-1060-1
  • Type

    conf

  • DOI
    10.1109/SIBCON.2013.6693577
  • Filename
    6693577