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
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