首页> 外文会议>Conference on Millimeter and Submillimeter Detectors for Astronomy, Aug 25-28, 2002, Waikoloa, Hawaii, USA >Design and fabrication of two-dimensional semiconducting bolometer arrays for the High resolution Airborne Wideband Camera (HAWC) and the Submillimeter High Angular Resolution Camera II (SHARC- II)
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Design and fabrication of two-dimensional semiconducting bolometer arrays for the High resolution Airborne Wideband Camera (HAWC) and the Submillimeter High Angular Resolution Camera II (SHARC- II)

机译:高分辨率机载宽带相机(HAWC)和亚毫米高角度分辨率相机II(SHARC-II)的二维半导体辐射热计阵列的设计和制造

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The High resolution Airborne Wideband Camera (HAWC) and the Submillimeter High Angular Resolution Camera II (SHARCII) will use almost identical versions of an ion-implanted silicon bolometer array developed at the National Aeronautics and Space Administration's Goddard Space Flight Center (GSFC). The GSFC "Pop-Up" Detectors (PUD's) use a unique folding technique to enable a 12 x 32-element close-packed array of bolometers with a filling factor greater than 95 percent. A kinematic Kevlar~R suspension system isolates the 200 mK bolometers from the helium bath temperature, and GSFC ― developed silicon bridge chips make electrical connection to the bolometers, while maintaining thermal isolation. The JFET preamps operate at 120 K. Providing good thermal heat sinking for these, and keeping their conduction and radiation from reaching the nearby bolometers, is one of the principal design challenges encountered. Another interesting challenge is the preparation of the silicon bolometers. They are manufactured in 32-element, planar rows using Micro Electro Mechanical Systems (MEMS) semiconductor etching techniques, and then cut and folded onto a ceramic bar. Optical alignment using specialized jigs ensures their uniformity and correct placement. The rows are then stacked to create the 12 x 32-element array. Engineering results from the first light run of SHARC II at the Caltech Submillimeter Observatory (CSO) are presented.
机译:高分辨率机载宽带摄像头(HAWC)和亚毫米高角度分辨率摄像头II(SHARCII)将使用由美国航空航天局戈达德太空飞行中心(GSFC)开发的几乎相同版本的离子注入硅测辐射热计阵列。 GSFC“弹出式”检测器(PUD)使用独特的折叠技术,可实现填充系数大于95%的12 x 32元素密排辐射热计阵列。运动学的Kevlar〜R悬挂系统将200 mK测辐射热计与氦浴温度隔离开来,并且GSFC开发的硅桥芯片与测辐射热计进行电气连接,同时保持热隔离。 JFET前置放大器的工作温度为120K。为这些放大器提供良好的散热性能,并防止其传导和辐射到达附近的辐射热计,是遇到的主要设计挑战之一。另一个有趣的挑战是硅辐射热计的制备。它们使用微机电系统(MEMS)半导体蚀刻技术制成32元素的平面行,然后切割并折叠到陶瓷棒上。使用专用夹具进行光学对准可确保其均匀性和正确放置。然后将这些行堆叠起来以创建12 x 32元素的数组。介绍了Caltech亚毫米天文台(CSO)进行的SHARC II首次试运行的工程结果。

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