Shirron Peter J, Kimball Mark O, James Bryan L, Muench Theodore, Canavan Edgar R, DiPirro Michael J, Bialas Thomas A, Sneiderman Gary A, Boyce Kevin R, Kilbourne Caroline A, Porter Frederick S, Fujimoto Ryuichi, Takei Yoh, Yoshida Seiji, Mitsuda Kazuhisa
NASA/Goddard Space Flight Center, Greenbelt, MD, USA 20771.
Kanazawa University, Kanazawa, Ishikawa 920-1192, Japan.
J Astron Telesc Instrum Syst. 2018 Apr;4(2). doi: 10.1117/1.JATIS.4.2.021403.
The Soft X-ray Spectrometer (SXS) instrument that flew on the Astro-H observatory was designed to perform imaging and spectroscopy of x-rays in the energy range of 0.2 to 13 keV with a resolution requirement of 7 eV or better. This was accomplished using a 6x6 array of x-ray microcalorimeters cooled to an operating temperature of 50 mK by an adiabatic demagnetization refrigerator (ADR). The ADR consisted of three stages in order to operate using either a 1.2 K superfluid helium bath or a 4.5 K Joule-Thomson (JT) cryocooler as its heat sink. The design was based on the following operating strategy. After launch, while liquid helium was present (cryogen mode), two of the ADR's stages would be used to single-shot cool the detectors, using the helium as a heat sink. When the helium was eventually depleted (cryogen-free mode), all three ADR stages would be used to continuously cool the helium tank to about 1.5 K, and to single-shot cool the detectors (to 50 mK), using the JT cryocooler as a heat sink. The Astro-H observatory, renamed Hitomi after its successful launch in February 2016, carried approximately 36 liters of helium into orbit. Based on measurements during ground testing, the average heat load on the helium was projected to be 0.66 mW, giving a lifetime of more than 4 years. On day 5, the helium had cooled to <1.4 K and ADR operation began, successfully cooling the detector array to 50 mK. The ADR's hold time steadily increased to 48 hours as the helium cooled to a temperature of 1.12 K. As the commissioning phase progressed, the ADR was recycled (requiring approximately 45 minutes) periodically, either in preparation for science observations or whenever the 50 mK stage approached the end of its hold time. In total, 18 cycles were completed by the time an attitude control anomaly led to an unrecoverable failure of the satellite on day 38. This paper presents the design, operation and on-orbit performance of the ADR in cryogen mode as the foreshortened mission did not provide an opportunity to test cryogen-free mode.
搭载于“天体-H”天文台的软X射线光谱仪(SXS)旨在对能量范围为0.2至13千电子伏特的X射线进行成像和光谱分析,分辨率要求达到7电子伏特或更高。这是通过一个6×6的X射线微热量计阵列实现的,该阵列由绝热去磁制冷机(ADR)冷却至50毫开尔文的工作温度。ADR由三个阶段组成,以便使用1.2开尔文的超流氦浴或4.5开尔文的焦耳-汤姆逊(JT)低温制冷机作为其散热器运行。该设计基于以下运行策略。发射后,当存在液氦时(低温剂模式),ADR的两个阶段将用于单次冷却探测器,以氦作为散热器。当氦最终耗尽时(无低温剂模式),所有三个ADR阶段将用于将氦罐连续冷却至约1.5开尔文,并单次冷却探测器(至50毫开尔文),以JT低温制冷机作为散热器。“天体-H”天文台在2016年2月成功发射后更名为“瞳”,携带了约36升氦进入轨道。根据地面测试期间的测量,氦上的平均热负荷预计为0.66毫瓦,寿命超过4年。在第5天,氦冷却至<1.4开尔文,ADR开始运行,成功将探测器阵列冷却至50毫开尔文。随着氦冷却至1.12开尔文的温度,ADR的保持时间稳步增加至48小时。随着调试阶段的推进,ADR会定期循环(需要约45分钟),要么是为科学观测做准备,要么是每当50毫开尔文阶段接近其保持时间结束时。到第38天姿态控制异常导致卫星出现不可恢复的故障时,总共完成了18个循环。由于缩短的任务没有提供测试无低温剂模式的机会,本文介绍了ADR在低温剂模式下的设计、运行和在轨性能。