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Characterization of the JWST Pathfinder mirror dynamics using the center of curvature optical assembly (CoCOA)

机译:利用曲率中心(Cocoa)的JWST Pathfinder镜像动力学的表征

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The James Webb Space Telescope (JWST) Optical Telescope Element (OTE) consists of a 6.6 m clear aperture, 18 segment primary mirror, all-reflective, three-mirror anastigmat operating at cryogenic temperatures. To verify performance of the primary mirror, a full aperture center of curvature optical null test is performed under cryogenic conditions in Chamber A at the National Aeronautics and Space Administration (NASA) Johnson Space Center (JSC) using an instantaneous phase measuring interferometer. After phasing the mirrors during the JWST Pathfinder testing, the interferometer is utilized to characterize the mirror relative piston and tilt dynamics under different facility configurations. The correlation between the motions seen on detectors at the focal plane and the interferometer validates the use of the interferometer for dynamic investigations. The success of planned test hardware improvements will be characterized by the multi-wavelength interferometer (MWIF) at the Center of Curvature Optical Assembly (CoCOA).
机译:James Webb Space望远镜(JWST)光学望远镜元件(OTE)由6.6米的透明光圈,18个段初级镜,全反射三镜子Anastigmat进行,在低温温度下运行。为了验证主镜的性能,使用瞬时相位测量干涉仪在国家航空和空间管理(NASA)Johnson Space Center(JSC)的阴道内的低温条件下进行全光圈曲率光学空测试。在JWST探测器测试期间逐次相位后,干涉仪用于在不同设施配置下表征镜子相对活塞和倾斜动力学。在焦平面和干涉仪处的检测器上看到的动作之间的相关性验证了干涉仪以进行动态调查的使用。计划测试硬件改进的成功将在曲率光学组件(Cocoa)中的多波长干涉仪(MWIF)的特征征。

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