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

机译:Micro-X探测火箭X射线望远镜的进展:飞行硬件完成

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Micro-X is a rocket-borne X-ray telescope which will use an array of Transition Edge Sensor (TES) microcalorimetersto obtain high resolution soft X-ray spectra of extended astronomical sources. The microcalorimeter array consists of128 pixels with a size of 590 m x 590 m each. The TESs are read out with a time-division Superconducting QuantumInterference Device (SQUID) multiplexing system. The instrument's front end assembly, which contains themicrocalorimeter array and two SQUID amplification stages, is located at the focal point of a conically approximatedWolter mirror with a focal length of 2100 mm and a point spread function of 2.4 arcmin half-power diameter. Thetelescope's effective area amounts to 300 cm~2at 1 keV. The TES array is cooled with an Adiabatic DemagnetizationRefrigerator. The first flight of Micro-X is scheduled for 2011, and will likely target a Si knot in the Puppis A supernovaremnant. The time available for the observation above an altitude of 160 km will be in excess of 300 seconds. Thedesign, 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:微-X是将使用过渡边缘传感器(TES)的阵列microcalorimetersto获得的扩展天文源高分辨率软X射线光谱的箭载X射线望远镜。微量量热仪阵列由of128像素尺寸为590米每个x590米。的TESS与时分超导QuantumInterference器件(SQUID)复用系统读出。该仪器的前端组件,它包含themicrocalorimeter阵列和两个SQUID放大级,位于锥形approximatedWolter镜与2100毫米的焦距和2.4弧分半功率直径的点扩散函数的焦点。 Thetelescope的有效面积达300厘米〜2原子1千电子伏。的TES阵列与绝热DemagnetizationRefrigerator冷却。微-X的首次飞行定于2011年,并可能会针对在船尾座A supernovaremnant一个硅结。可用于160公里的高度上方的观测时间会超过300秒。 Thedesign,制造和装配飞行硬件最近已经完成,测试和系统测试是underway.We描述该项目的整体状态微-X设备的最终设计,并提出报告。

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