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XRS low temperature cryogenic system: Ground performance tests results

机译:XRS低温低温系统:地面性能测试结果

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摘要

The X-Ray Spectrometer (XRS) instrument is part of tile Astro-E mission scheduled to launch early in 2000. Its cryogenic system is required to cool a 32-clement array of X-ray microcalorimeters to 60-65 mK over a mission lifetime of at least 2 years. This is accomplished using an adiabatic demagnetization refrigerator (ADR) contained within a two-stage superfluid helium/solid neon cooler. Goddard Space Flight Center is providing the ADR and helium dewar. The flight helium dewar was assembled in Sept. 1997 and subjected to extensive thermal performance tests. This paper presents test results at both the subsystem and component levels. In addition, results of the low temperature topoff performed in Japan with the engineering unit neon and helium dewars are discussed.
机译:X射线光谱仪(XRS)仪器是计划于2000年初发射的瓦特Astro-E任务的一部分。其低温系统需要在任务寿命内将32片X射线微热量计阵列冷却至60-65 mK至少2年。这是通过两级超流氦/固体氖冷却器中装有的绝热去磁制冷机(ADR)实现的。戈达德太空飞行中心正在提供ADR和氦杜瓦瓶。飞行氦杜瓦瓶于1997年9月组装,并进行了广泛的热性能测试。本文介绍了子系统和组件级别的测试结果。另外,还讨论了在日本使用氖和氦杜瓦瓶进行工程制做的低温补给结果。

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