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Carbon-carbon composite: a strong material with low thermal conductivity and thermal contact for rigid optical assemblies at low temperature

✍ Scribed by C. Blondel; R. Roquessalane; O.A. Testard; F. Latimier; D. Viratelle


Publisher
Elsevier Science
Year
1989
Tongue
English
Weight
264 KB
Volume
29
Category
Article
ISSN
0011-2275

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✦ Synopsis


The temperature of the European Space Infrared Telescope ISO (Infrared Space Observatory) was optimized at 1.8 K for actual cryogenic design. Some of the detector parts of the instrumentation can have a different optimal thermalization but they are also very strongly fixed, all with the smallest thermocontrol budget and respecting strong vibration constraints. As an analysis of data, carbon-carbon composite, available locally, was qualified as the best present solution to this problem.