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Icy Target Thermal Test Apparatus and Calibration of a Planetary Spectrometer

机译:冰冷的目标热试验装置和行星光谱仪的校准

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The Compositional Infrared Imaging Spectrometer (CIRIS) is currently under development at JPL for outer planetary missions, and is undergoing thermal-vacuum environmental testing as part of the TRL progression effort. This involves analyzing icy targets under cryogenic vacuum conditions with the spectrometer and the use of an optical calibration device designed for integration with the test setup. CIRIS was designed for use on a future Europa orbiter, with applications for missions to other worlds including Mars. It has a compact and rugged design due to its spinning refractor, which replaces the moving mirror setup of a traditional Michelson interferometer. We have designed and fabricated a test apparatus to calibrate CIRIS using a black body source and to measure reflectance of ice specimens. The apparatus presented here is validating the performance of CIRIS under Europa-like conditions, including temperature of the spectrometer, temperature of the target, and illumination of the target. A dewar assembly resides inside the vacuum chamber and is filled with liquid nitrogen using a fluid feedthrough. A cold plate mounted directly to the dewar will freeze/ contain the ice or rock targets. An external blackbody light source will illuminate the targets via a mirror/ window assembly, and a second mirror will direct the reflected light into the spectrometer. The mirror configuration can be moved in six degrees of freedom for optical alignment. The calibration source is designed to emit blackbody radiation at known and controllable temperatures between 150 and 350K via interchangeable apertures. To maintain an emissivity as close as possible to that of an ideal blackbody, the calibration source is a conical cavity coated with highly emissive paint within a solid cylinder. The cavity is made of aluminum and contains multiple heaters to ensure isothermal conditions, with ceramic standoffs to create a long thermal path which allows the cavity to be at a high temperature while the spectrometer and other nearby hardware remain cryogenic.
机译:组成红外成像光谱仪(CIRIS)目前正在JPL进行外行星任务的开发,并作为TRL进展工作的一部分进行热真空环境测试。这涉及在低温真空条件下分析冰冷的靶,并使用设计用于与测试设置集成的光学校准装置。 CiRIS专为未来的Europa Orbiter使用,申请代码申请到包括火星在内的其他世界。由于其纺纱折射器,它具有紧凑且坚固的设计,该设计取代了传统迈克尔森干涉仪的移动镜设置。我们已经设计和制造了使用黑色体源校准CIRIS的测试设备,并测量冰标本的反射率。本文介绍的该装置是验证CiRIS在欧罗巴样条件下的性能,包括光谱仪的温度,靶标的温度和靶的照明。杜瓦组件在真空室内置于真空室内,使用流体馈通填充有液氮。直接安装在杜瓦尔的冷板将冻结/含有冰或岩石靶标。外部黑体光源将通过镜子/窗口组件亮起目标,第二镜将反射光引导到光谱仪中。镜子配置可以以六个自由度移动用于光学对准。校准源设计成通过可互换的孔在150至350k之间的已知和可控温度下发射黑体辐射。为了保持尽可能靠近理想的黑体的发光率,校准源是涂有固体圆筒内的高发光涂料的锥形腔。腔由铝制成,含有多个加热器,以确保等温条件,陶瓷支架形成长的热路径,使腔体在高温下,同时光谱仪和其他附近的硬件保持低温。

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