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Determining the Optimum Energy Performance of an On-Board Cryogenic Cooler

Dmitriy A. Uglanov, Viktor V Urlapkin, Sergey S Korneev, and Elizaveta A. Marakhova
The Institute of Engines and Power Plants of the Samara National Research University, Department of Heat Engineering and Heat Engines Samara, Russia
Abstract—This work solves the problem of reducing the loss of a cryoproduct during its storage on board a spacecraft by using a special cooling system. A calculation is carried out to compare cooling systems such as a throttle cooling system, a gas cryogenic Stirling machine and an air refrigeration unit. Comparing the calculated parameters of the systems, an optimal cooling system was selected for storing cryoproducts on board the spacecraft.


Index Terms—reduction of cryogenic product losses, cryogenic fuel, cooling system, Lorenz cycle, air refrigeration unit, Stirgling cycle, throttle cooling system

Cite: Dmitriy A. Uglanov, Viktor V Urlapkin, Sergey S Korneev, and Elizaveta A. Marakhova, "Determining the Optimum Energy Performance of an On-Board Cryogenic Cooler," Journal of Automation and Control Engineering, Vol. 9, No. 1, pp. 1-8, June, 2021. doi: 10.18178/joace.9.1.1-8
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