• DocumentCode
    3514524
  • Title

    High Speed RF Packaging Design and Fabrication for Ka-Band Radar Systems

  • Author

    Gontijo, Ivair

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    The various choices of materials for RF packaging are reviewed and two groups of materials are used to package components for a Ka-band landing radar. A Kovar housing was designed and built for a transmit/receive module, which provides good RF performance and allows the high power semiconductor amplifiers to be mounted directly to pedestals at the bottom of the package. For the up/down converter, an Aluminum housing was designed and built with all connectors laser welded in place. Both packages are hermetic and capable of withstanding a differential pressure of over 30 psi. Environmental requirements are taken into consideration during package design, such as thermal cycling, absolute maximum temperature ratings of components and structural aspects. Details of the electrical package design to minimize radiation loss and cross talk are discussed, as well as various methods of attachment of the RF connectors to the housings.
  • Keywords
    crosstalk; electronics packaging; microwave devices; millimetre wave devices; radar receivers; radar transmitters; Ka-band radar systems; Kovar housing; RF connectors; high power semiconductor amplifiers; high speed RF packaging; landing radar; maximum temperature ratings; radiation loss; thermal cycling; Aluminum; Connectors; Fabrication; High power amplifiers; Radar; Radio frequency; Radiofrequency amplifiers; Semiconductor device packaging; Semiconductor materials; Semiconductor optical amplifiers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526477
  • Filename
    4526477