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Progress on the Micro-X sounding rocket X-ray telescope:completion of flight hardware

机译:Micro-X探空火箭X射线望远镜的进展:飞行硬件的完成

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Micro-X is a rocket-borne X-ray telescope which will use an array of Transition Edge Sensor (TES) microcalorimeters to obtain high resolution soft X-ray spectra of extended astronomical sources. The microcalorimeter array consists of 128 pixels with a size of 590 μm × 590 μm each. The TESs are read out with a time-division Superconducting Quantum Interference Device (SQUID) multiplexing system. The instrument's front end assembly, which contains the microcalorimeter array and two SQUID amplification stages, is located at the focal point of a conically approximated Wolter mirror with a focal length of 2100 mm and a point spread function of 2.4 arcmin half-power diameter. The telescope's effective area amounts to ~300 cm~2 at 1 keV. The TES array is cooled with an Adiabatic Demagnetization Refrigerator. The first flight of Micro-X is scheduled for 2011, and will likely target a Si knot in the Puppis A supernova remnant. The time available for the observation above an altitude of 160 km will be in excess of 300 seconds. The design, manufacturing and assembly of the flight hardware has recently been completed, and system testing is underway. We describe the final design of the Micro-X instrument, and report on the overall status of the project.
机译:Micro-X是一枚火箭X射线望远镜,它将使用一系列的过渡边缘传感器(TES)量热仪来获得扩展的天文源的高分辨率软X射线光谱。微热量计阵列由128个像素组成,每个像素的大小为590μm×590μm。使用时分超导量子干扰设备(SQUID)多路复用系统读取TES。该仪器的前端组件包括一个微热量计阵列和两个SQUID放大级,位于圆锥形近似Wolter反射镜的焦点处,其焦距为2100 mm,点扩散函数为2.4 arcmin半功率直径。 1 keV时,望远镜的有效面积约为〜300 cm〜2。 TES阵列用绝热退磁冰箱冷却。 Micro-X的首次飞行定于2011年进行,很可能瞄准Puppis A超新星残骸中的Si结。在海拔160公里以上进行观测的时间将超过300秒。飞行硬件的设计,制造和组装最近已经完成,并且系统测试正在进行中。我们描述了Micro-X仪器的最终设计,并报告了该项目的总体状况。

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