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ATHENA X-IFU 300?K-50?mK cryochain demonstrator cryostat

机译:Athena X-IFU 300?K-50?MK Cryochain Sextrator Cryostat

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In the framework of the ESA X-ray mission ATHENA, scheduled for launch in 2028, an ESA Core Technology Program (CTP) was started in 2016 to build a flight like cryostat demonstrator in parallel with the phase A studies of the ATHENA/X-IFU instrument . As part of this CTP, called the Detector Cooling System (DCS), design, manufacturing and test of a cryostat including existing space coolers will be done. In addition to the validation of thermal performance, a Focal Plan Assembly (FPA) demonstrator using Transition Edge Sensors (TES) detector technology will be also integrated and its performance characterized versus the environment provided by the cryostat. This is a unique opportunity to validate many crucial issues of the cryogenic part of such a sensitive instrument.A dedicated activity within this CTP-DCS is the demonstration of the 300?K–50?mK cooling chain in a Ground System Equipment (GSE) cryostat. The studies are focused on the operation of the space coolers, which is made possible by the use of a ground cooler for cooling cryogenic shields and mechanical supports. Thanks to the modularity of the cryostat, several cooling chains could be tested. In the base line configuration described here, the low temperature stage is the CEA hybrid sorption/ADR 50?mK cooler with thermal interfaces at 4?K and 2?K. 4?K cooling is accomplished by a 4?K Joule-Thomson (JT) cryocooler and its Stirling precooler provided by JAXA. Regarding the 2?K stage, at first a 2?K?JT from JAXA will be used. Alternatively, a 2?K?JT cooler from RAL could replace the JAXA 2?K?JT. In both cases new prototype(s) of a 2?K?JT will be implemented, precooled by the EM 15?K pule tube cooler from Air Liquide. This test program is also the opportunity to validate the operation of the cryochain with respect to various requirements, such as time constant and temperature stabilities. This would bring us valuable inputs to integrate the cryochain in DCS cryostat or for the X-IFU phase A studies. This cryochain demonstration is also a critical milestone for the SPICA mission . The design of the cryostat and first thermal validations both before and after integration of the JAXA JT coolers are presented in this paper.
机译:在ESA X-Ray Mission Athena的框架中,计划于2028年推出,2016年开始了ESA核心技术计划(CTP),以与雅典娜/ X-的研究相阶段平行地建造像Cryostat Sextator这样的航班IFU仪器。作为该CTP的一部分,称为检测器冷却系统(DCS),将完成包括现有空间冷却器的低温仪的设计,制造和测试。除了验证热性能之外,还将综合规划组件(FPA)演示器使用过渡边缘传感器(TES)检测器技术还集成,其性能表征与低温恒温器提供的环境。这是验证这种敏感仪器的低温部分的许多关键问题的独特机会。该CTP-DCS中的专用活动是300?K-50?MK冷却链中的300?MK冷却链(GSE)。低温恒温器。这些研究专注于空间冷却器的操作,这是通过使用用于冷却低温屏蔽和机械支撑的地面冷却器来实现的。由于低温恒温器的模块化,可以测试几个冷却链。在这里描述的基线配置中,低温阶段是CEA混合吸附/ ADR 50?MK冷却器,其热界面处为4Ω·k和2?k。 4?k冷却由4?K焦耳 - 汤姆森(JT)冷冻室及其由JAXA提供的斯特林预冷却器完成。关于2?k阶段,起初2?k?来自Jaxa的JT。或者,来自RAL的2?K?JT冷却器可以取代JAXA 2?K 2 JT。在这两种情况下,将实现2?K的新原型。将通过来自空气液化的EM 15?K Pule管冷却器来实现。该测试程序也是有机会验证干酪棘关于各种要求的操作,例如时间恒定和温度稳定性。这将为我们提供有价值的投入,以将干酪氏橡胶的融合在DCS Cryostat中或X-IFU阶段集成。这个干冰船示范也是SPICA任务的关键里程碑。在本文中提出了jaxaJT冷却器的集成之前和之后的低温恒温器和第一热验证。

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