ShareDemonstration of low temperature radiative cooler for future space missions.
Author(s) : CUSHMAN G. M., MATHER J. C., FIXSEN D. J.
Type of article: Article
Summary
A miniature radiative cooler was designed, constructed, and tested and achieved a stabilized temperature of 34 K with no load and an outer shell temperature of 91 K. This is an improvement upon previous lower limits of radiative coolers of 50 K. Thermal modelling and experiment agree within 2 K.
Details
- Original title: Demonstration of low temperature radiative cooler for future space missions.
- Record ID : 1998-2709
- Languages: English
- Source: Rev. sci. Instrum. - vol. 68 - n. 12
- Publication date: 1997/12
- Document available for consultation in the library of the IIR headquarters only.
Links
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Indexing
- Themes: Other applications of cryogenic temperatures
- Keywords: Radiation; Manufacture; Design; Miniaturization; Testing; Space; Cryocooler
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