• DocumentCode
    2700751
  • Title

    Pick-up horn for high power TVAC test of spacecraft payloads for communication satellites

  • Author

    Rao, Sudhakar ; Lee-Yow, Clency ; Venezia, Philip

  • Author_Institution
    Lockheed Martin Commercial Space Syst., Newtown, PA
  • fYear
    2006
  • fDate
    9-14 July 2006
  • Firstpage
    3133
  • Lastpage
    3136
  • Abstract
    This paper presents a novel method for high power thermal vacuum tests of spacecraft payloads using pick-up horns (PUH). The PUH method has benefits of being cost-effective, compact, easy to implement, does not require breaking the vacuum several times and avoids physical contact with flight hardware. It is designed with four oversized slots to receive the high RF power from the flight horns, absorb almost all the power and efficiently transfer the heat outside the TVAC chamber with minimal reflections back to the horn and minimal RF leakage outside the PUH. The PUH has been successfully used for high power TVAC testing and validation of a Ku-band payload for satellite communications
  • Keywords
    antenna testing; microwave antennas; satellite antennas; Ku-band payload; RF leakage; flight hardware; flight horns; high RF power; high power TVAC test; high power thermal vacuum tests; pick-up horn; satellite communication; spacecraft payloads; Artificial satellites; Coolants; Hardware; Heat transfer; Payloads; Performance evaluation; Radio frequency; Reflection; Space vehicles; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Antennas and Propagation Society International Symposium 2006, IEEE
  • Conference_Location
    Albuquerque, NM
  • Print_ISBN
    1-4244-0123-2
  • Type

    conf

  • DOI
    10.1109/APS.2006.1711274
  • Filename
    1711274