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50 mK cooling solution with an ADR precooled by a sorption cooler

机译:50 mK冷却液,带有由吸附式冷却器预冷的ADR

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摘要

CEA/SBT is currently developing a 2.5 K-50 mK cooling solution composed of a small demagnetization refrigerator (ADR) precooled by a sorption cooler, equivalent to the high temperature stage of a two-stage ADR system. Thanks to the use of this dual technology, a low weight cooler able to reach 50 mK with a heat sink up to 2.5 K can be designed. Because the sorption cooler is probably the lightest solution to produce sub-Kelvin temperatures, these developments allow us to propose a solution to face the drastic reduction in the mass budget of space missions like SPICA or IXO. The European Space Agency (ESA) is funding the development of an engineering model able to produce 1 μW net heat lift at 50 mK. It is sized so that the sorption cooler provides an additional 10 μW at 300 mK. The ESA main requirements are anautonomy of more than 24 h and a recycling time smaller than 8 h. We present the design of the system able to meet these requirements as well as the expected performances and preliminary measurements.
机译:CEA / SBT当前正在开发一个2.5 K-50 mK的冷却解决方案,该解决方案由一个小型的去磁制冷机(ADR)组成,该制冷机由吸附冷却器预冷却,相当于两级ADR系统的高温阶段。由于采用了这种双重技术,因此可以设计出一种重量轻的冷却器,该冷却器能够达到50 mK,并具有高达2.5 K的散热片。由于吸收式冷却器可能是产生低于开尔文温度的最轻的解决方案,因此这些发展使我们能够提出一种解决方案,以应对诸如SPICA或IXO之类的太空飞行任务的大量预算急剧减少。欧洲航天局(ESA)正在资助一种工程模型的开发,该模型能够在50 mK时产生1 W的净热升力。它的大小使吸收式冷却器在300 mK时提供额外的10μW。 ESA的主要要求是自主时间超过24小时,回收时间少于8小时。我们介绍了能够满足这些要求以及预期性能和初步测量的系统设计。

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