Several NASA programmes designed to monitor the earth's atmosphere fro
m space utilize infrared detectors which operate at or below 4.2 K for
optimum performance. At present, the detectors are maintained at cryo
genic temperatures by a stored volume of liquid helium. These detector
s must be electrically linked to amplification electronics and data st
orage instruments maintained at 80 K. The electrical connections over
the temperature gradient account for approximate to 20% of the total h
eat load on the Dewar for some systems, accelerating the boil-off of l
iquid helium cryogen and reducing the operational lifetime of the spac
e-borne instruments. The recent discovery of high temperature supercon
ductors has provided an opportunity to develop electrically conductive
, thermally insulating links to bridge this thermal gradient. This pap
er describes the modelling of the thermal transport properties of thic
k film, high T-c electrical bridges across a 4.2-80 K temperature grad
ient and the impact of such devices on a spaceborne remote sensing sys
tem.