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Cryogenic Heat Transfer System
- Publication Year :
- 2018
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 2018.
-
Abstract
- Disclosed herein is a cryogenic heat transfer system capable of transferring 50 W or more at cryogenic temperatures of 100.degree. K or less for use with cryocooler systems. In an embodiment, a cryogenic heat transfer system comprises a refrigerant contained within an inner chamber bound by a condenser in fluid communication with an evaporator through at least one flexible conduit, the condenser in thermal communication with the cold station of a cryocooler, and the evaporator positionable in thermal communication with a heat source, typically a radiation shield of a cryogenic chamber. A process to remove heat from a cryogenic chamber is also disclosed.
- Subjects :
- Fluid Mechanics And Thermodynamics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NNN12AA01C
- Publication Type :
- Report
- Accession number :
- edsnas.20190000744
- Document Type :
- Report