论文标题
Olimpo Balloon的长期低温系统 - 传播实验:设计和 - 飞行性能
The long duration cryogenic system of the OLIMPO balloon--borne experiment: design and in--flight performance
论文作者
论文摘要
我们描述了低温恒温器的设计和内在性能以及用于Olimpo Balloon-Borne-Borne实验的冰箱,这是一种测量星系簇中Sunyaev-Zel'Dovich效应的分光光度计。 $^{3} $ He冰箱为四个阵列的四个动力电感探测器提供了0.3 K的操作温度,该探测器以150、250、350和460 GHz为中心的4个频段。低温恒温器为$^{3} $冰箱提供了1.65 K的基本温度,并在约2 k处冷却了重新成像的光学元件和过滤器链。 该集成系统的设计约为15天,以实现计划中的Olimpo观测值所需的灵敏度,并在2018年7月Olimpo的第一次长期平流层飞行中成功操作。 低温恒温器具有两个水箱,一个用于液氮,另一个用于液态氦气。通过定制的僵硬的G10玻璃纤维管支撑实现了长时间的时间,从而确保了低导热率和显着的结构刚度。多层超级绝位和蒸气冷却屏蔽层,全部减少了液态氦气罐上的热负荷。 该系统在实验室进行了测试,无人操作超过15天,然后在平流层的长时间持续时间飞行中进行了测试。在这两种情况下,检测器温度均低于300 mk,热稳定性优于$ \ pm $ 0.5 mk。 该系统还在漫长的持续时间平流层气球飞行中成功运行。
We describe the design and in--flight performance of the cryostat and the self-contained $^{3}$He refrigerator for the OLIMPO balloon--borne experiment, a spectrophotometer to measure the Sunyaev-Zel'dovich effect in clusters of galaxies. The $^{3}$He refrigerator provides the 0.3 K operation temperature for the four arrays of kinetic inductance detectors working in 4 bands centered at 150, 250, 350 and 460 GHz. The cryostat provides the 1.65 K base temperature for the $^{3}$He refrigerator, and cools down the reimaging optics and the filters chain at about 2 K. The integrated system was designed for a hold time of about 15 days, to achieve the sensitivity required by the planned OLIMPO observations, and successfully operated during the first long-duration stratospheric flight of OLIMPO in July 2018. The cryostat features two tanks, one for liquid nitrogen and the other one for liquid helium. The long hold time has been achieved by means of custom stiff G10 fiberglass tubes support, which ensures low thermal conductivity and remarkable structural stiffness; multi--layer superinsulation, and a vapour cooled shield, all reducing the heat load on the liquid helium tank. The system was tested in the lab, with more than 15 days of unmanned operations, and then in the long duration balloon flight in the stratosphere. In both cases, the detector temperature was below 300 mK, with thermal stability better than $\pm$ 0.5 mK. The system also operated successfully in the long duration stratospheric balloon flight.