A 4 K pulse tube cryocooler for the HUBS mission

Liubiao Chen, Z. Gao, Biao Yang, Junjie Wang
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Abstract

The Hot Universe Baryon Surveyor (HUBS) mission requires a refrigeration system with temperatures below 100 mK to meet the high-resolution detection requirements of its superconducting transition edge sensor. The refrigeration scheme is to use a 4 K mechanical cryocooler as the pre-cooling stage and then use adiabatic demagnetization refrigerators (ADR) to obtain mK temperatures. One option for the pre-cooling stage is to use a pulse tube cryocooler. At present, a thermalcoupled and gas-coupled composite prototype based on helium-4 as the working gas has been successfully developed, a no-load temperature of 3.1 K, and a maximum cooling capacity of 22.0 mW at 4.2 K has been obtained, which can barely meet the demand. The calculation results show that the use of helium-3 instead of helium-4 as the working gas of the gas-coupled second and third stage is expected to further increase the cooling capacity to 53.1mW/4.2K, but 53 standard liters of helium-3 needs to be charged at room temperature. In order to reduce the amount of helium-3, a thermal-coupled three-stage pulse tube cryocooler is further designed. When the first and second compressors and their cold fingers use helium-4, while the third compressor and its cold finger use helium-3 as the working gas, the calculation results show that a cooling capacity of 57.5 mW/4.2 K can be obtained, and the amount of helium-3 that needs to be charged at room temperature is 11 standard liters, which effectively reduces the cost.
用于HUBS任务的4k脉冲管制冷机
热宇宙重子探测器(HUBS)任务需要一个温度低于100 mK的制冷系统,以满足其超导过渡边缘传感器的高分辨率检测要求。制冷方案采用4 K机械制冷机作为预冷级,再采用绝热退磁制冷机(ADR)获得mK温度。预冷阶段的一个选择是使用脉冲管制冷机。目前,以氦-4为工作气体的热耦合和气耦合复合样机已经研制成功,空载温度为3.1 K, 4.2 K时的最大制冷量为22.0 mW,基本不能满足需求。计算结果表明,用氦-3代替氦-4作为气联二、三级的工作气体,制冷量有望进一步提高到53.1mW/4.2K,但需要在室温下充入53标准升的氦-3。为了减少氦-3的用量,进一步设计了热耦合三级脉冲管制冷机。当第一、第二压缩机及其冷指使用氦-4,第三压缩机及其冷指使用氦-3作为工作气体时,计算结果表明,可获得57.5 mW/4.2 K的制冷量,在室温下需要充氦的量为11标准升,有效降低了成本。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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