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

机译:使用曲率中心光学组件(CoCOA)表征JWST Pathfinder镜动力学

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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~(1,2,3). 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:詹姆斯·韦伯太空望远镜(JWST)光学望远镜元件(OTE)包括一个6.6 m的透明光圈,18段主镜,全反射,三反射镜,在低温下工作。为了验证主镜的性能,美国国家航空航天局(NASA)约翰逊航天中心(JSC)在A室的低温条件下使用瞬时相位测量干涉仪对全孔径曲率中心光学零点进行了测试[1]。 ,2,3)。在JWST Pathfinder测试期间对镜进行调相后,利用干涉仪来表征在不同设施配置下镜的相对活塞和倾斜动力学特性。在焦平面上的检测器上看到的运动与干涉仪之间的相关性验证了干涉仪在动态研究中的使用。计划中的测试硬件改进的成功将以曲率光学组件中心(CoCOA)的多波长干涉仪(MWIF)为特征。

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