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Design Models for the Development of Helium-Carbon Sorption CryocoolersWe have developed models for predicting the performance of helium-based Joule-Thomson continuous-flow cryocoolers using charcoal-pumped sorption compressors. The models take as inputs the number of compressors, desired heat-lift, cold tip temperature, and available precooling temperature and provide design parameters as outputs. Future laboratory development will be used to verify and improve the models. We will present a preliminary design for a two-stage vibration-free cryocooler that is being proposed as part of a mid-infrared camera on NASA's Next Generation Space Telescope. Model predictions show that a 10 mW helium-carbon cryocooler with a base temperature of 5.5 K will reject less than 650 mW at 18 K. The total input power to the helium-carbon stage is 650 mW. These models, which run in MathCad and Microsoft Excel, can be coupled to similar models for hydrogen sorption coolers to give designs for 2-stage vibration-free cryocoolers that provide cooling from approximately 50 K to 4 K.
Document ID
20010000272
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
Lindensmith, Chris A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Ahart, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Bhandari, P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Wade, L. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Paine, C. G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2000
Subject Category
Engineering (General)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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