• DocumentCode
    281085
  • Title

    Spacecraft front-end technology

  • Author

    Hall, W.J. ; Cahill, R. ; Martin, R.J.

  • Author_Institution
    British Aerospace Space Systems Ltd., Bristol, UK
  • fYear
    1992
  • fDate
    33879
  • Firstpage
    42705
  • Lastpage
    42708
  • Abstract
    Spacecraft receivers require technologies which combine optimum RF performance with robustness and low mass, while meeting volume constraints. The adaptation to the spacecraft application is most significant in the instrument front-end, comprising antenna, antenna feed, and mixer. The millimetric band from 89 GHz upwards is currently characterised by the use of quasi-optical feeds and subharmonically pumped double sideband mixers. In recognition of the increasing need for ever higher operating frequencies, and the stringent mass/volume constraints associated in particular with spacecraft environments, BAe Space Systems has developed an appropriate set of accurate predictive design aids, which have been verified against hardware. A key front-end component whose design is significantly constrained by the spacecraft environment is the mixer. Subharmonically pumped double planar diodes are robust. Experimental work using air-bridged and solid coupling structures was undertaken, and typical performance parameters produced
  • Keywords
    CAD; antenna feeders; microwave measurement; mixers (circuits); radio receivers; space vehicles; BAe Space Systems; air-bridged coupling structures; antenna feed; double planar diodes; mass/volume constraints; predictive design aids; quasi-optical feeds; solid coupling structures; spacecraft front-end receiver; subharmonically pumped double sideband mixers;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Millimetre and Sub-Millimetre Wave Heterodyne Receivers, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    193606