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Strained-layer-superlattice-based compact thermal imager for the International Space Station

机译:国际空间站的应变层超晶格的紧凑型热成像仪

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The compact thermal imager (CTI) is a dual-band, strained-layer-superlattice (SLS) detector-based instrument that was installed on the exterior of the International Space Station (ISS) in conjunction with the third Robotic Refueling Mission 3 (RRM3) in 2018. The CTI serves as a pathfinder for future thermal infrared capability on Landsat. The CTI incorporates an SLS hybrid, a dual-band 3-5 and 8-10 mu m, electrically switchable, 320 x 256 array with 30 mu m(2) pixels, bonded to an Indigo ISC0903 Readout Integrated Circuit (ROIC). The telescope was built around an integrated detector cryocooler assembly developed under a NASA Small Business Innovative Research award with QmagiQ, LLC. The cooler is a Ricor K508 and the front-end optics is a custom-designed, doublet lens telescope with a 150 mm focal length. The ground resolution is 80 meters/pixel from the ISS altitude of 400 km. A filter creates two spectral channels from the dual bands, 3.3-5.4 and 7.8-10.2 mu m. The detector hybrid control electronics is a custom-developed system based on the Teledyne Imaging Systems SIDECAR Application-Specific Integrated Circuit. This module provides the electronic interface from the RRM3 SpaceCube on-board processor to the detector/ROIC assembly. The primary goal of this mission was to perform a technology demonstration of the SLS technology and the commercial cooler technology elevating the Technology Readiness Level (TRL) to TRL 9 on a bare-bones budget and relatively fast development cycle. Some science objectives include locating fires, approximating land surface temperatures, and monitoring evapo-transpiration, sea ice, and glacier dynamics. In this paper, we will present the design of the focal plane, optics, electronics, and mechanical structure of the CTI. We will also describe the operation and qualification tests that were performed to bring the CTI to the NASA TRL 6 in preparation for the launch on a SpaceX Dragon from the Kennedy Space Center. (C) 2019 Optical Society of America
机译:紧凑的热成像仪(CTI)是双频带,紧张层 - 超晶格(SLS)探测器的基于仪器,其安装在国际空间站(ISS)的外部,与第三机器人加油使命3(RRM3 )2018年。CTI用作兰德拉特的未来热红外能力的探测器。 CTI包括SLS混合,双频带3-5和8-10μm,电切换,320×256阵列,具有30μm(2)像素,绑定到Indigo ISC0903读出集成电路(ROIC)。望远镜围绕着由NASA小型企业创新研究奖的集成探测器冷冻室组装,与QMAGIQ,LLC开发。冷却器是RICOR K508,前端光学器件是一种定制设计的双峰镜头望远镜,焦距为150mm。地面分辨率为80米/像素,ISS高度为400公里。过滤器从双频带创建两个光谱通道,3.3-5.4和7.8-10.2 mu m。检测器混合控制电子设备是一种基于Teledyne成像系统Sidecar应用专用集成电路的定制系统。该模块将来自RRM3 Spacecube车载处理器的电子接口提供给探测器/ ROIC组件。该特派团的主要目标是执行SLS技术的技术演示和商业较低的技术在裸骨预算和相对较快的开发周期上提升技术准备水平(TRL)到TRL 9。一些科学目标包括定位火灾,近似土地表面温度和监测蒸发蒸腾,海冰和冰川动态。在本文中,我们将介绍CTI的焦平面,光学,电子产品和机械结构的设计。我们还将描述为将CTI带到NASA TRL 6的操作和资格测试,以准备从肯尼迪航天中心的Spacex Dragon发射。 (c)2019年光学学会

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