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Large Area Cryocooling for Far Infrared Telescopes

机译:远红外望远镜的大面积低温冷却

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Requirements for cryocooling of large-area heat sources begin to appear in studies of future space missions. Examples are the cooling of (i) the entire structure/mirror of large Far Infrared space telescopes to 4-40K and (ii) cryogenic thermal bus to maintain High Temperature Superconductor electronics to below 75K. The cryocooling system must provide robust/reliable operation and not cause significant vibration to the optical components. But perhaps the most challenging aspect of the system design is the removal of waste heat over a very large area. A cryogenic Loop Heat Pipe (C-LHP)/ cryocooler cooling system was developed with the ultimate goal of meeting the aforementioned requirements. In the proposed cooling concept, the C-LHP collected waste heat from a large-area heat source and then transported it to the cryocooler coldfinger for rejection. A proof-of-concept C-LHP test loop was constructed and performance tested in a vacuum chamber to demonstrate the feasibility of the proposed C-LHP to distribute the cryocooler cooling power over a large area. The test loop was designed to operate with any cryogenic working fluid such as Oxygen/Nitrogen (60-120K), Neon (28-40K), Hydrogen (18-30K), and Helium (2.5-4.5K). Preliminary test results indicated that the test loop had a cooling capacity of 4.2W in the 30-40K temperature range with Neon as the working fluid.
机译:大面积热源冷冻冷却的要求开始出现在对未来太空任务的研究中。例如:将(i)大型远红外太空望远镜的整个结构/镜冷却至4-40K,以及(ii)低温热总线,以将高温超导体电子设备保持在75K以下。低温冷却系统必须提供坚固/可靠的操作,并且不会对光学组件造成明显的振动。但是,系统设计中最具挑战性的方面可能是在很大的区域内消除废热。开发了低温回路热管(C-LHP)/低温冷却器冷却系统,其最终目标是满足上述要求。在提出的冷却概念中,C-LHP从一个大面积的热源收集废热,然后将其传输到低温冷却器的冷指中进行剔除。构建了概念验证的C-LHP测试回路,并在真空室内进行了性能测试,以证明所建议的C-LHP在大面积上分配低温冷却器冷却功率的可行性。该测试回路设计为可与任何低温工作流体配合使用,例如氧气/氮气(60-120K),氖气(28-40K),氢气(18-30K)和氦气(2.5-4.5K)。初步测试结果表明,在以Neon为工作流体的情况下,该测试回路在30-40K温度范围内的冷却能力为4.2W。

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