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Optical assessment of the James Webb Space Telescope primary and secondary mirror cryogenic alignment with a Hartmann test

机译:利用Hartmann测试对James Webb空间望远镜的一次和二次反射镜低温对准进行光学评估

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The James Webb Space Telescope is a large, deployable telescope that will operate at cryogenic temperatures at the Earth-Sun Lagrange 2 point. The Webb Optical Telescope Element (OTE) consists of 18 actively controlled Primary Mirror Segment Assemblies (PMSAs), an actively controlled Secondary Mirror Assembly (SMA), and an Aft-Optics Subsystem (AOS) that contains a fixed Tertiary Mirror and a Fine Steering Mirror. The OTE is combined with the Integrated Science Instrument Module (ISIM) to create the full optical train called OTIS (OTE&ISIM).OTIS has recently undergone cryogenic vacuum testing in Chamber A at Johnson Space Center in Houston, TX. A key outcome of this test was to verify there is adequate range of motion in PMSA and SMA actuators to align them to AOS/ISIM under flight-like conditions. The alignment state of the PMSAs and SMA was measured using photogrammetry and cross-checked optically using a variation of a classical Hartmann test. In the "Pass-and-a-Half" (PAAH) configuration, fiber sources near the Cassegrain focus propagate light through the full optical train and small tilts on the PMSAs create an array of spots on the science instrument detectors, mimicking the effect of a Hartmann mask. Comparison of measured and modeled spot arrays provides the alignment state of the SMA and the global tilt of the primary mirror. This paper will discuss the methodology, testing, and analysis performed to measure the alignment state of OTIS using the Hartmann method and verify the primary and secondary mirrors can be successfully aligned on orbit to meet performance requirements.
机译:James Webb Space Telescope是一个大型可展开的望远镜,将在地球阳光拉格朗日2点的低温温度下运行。韦伯光学望远镜元件(OTE)由18个主动控制的主镜段组件(PMSAS),一个主动控制的二手镜组件(SMA),以及包含固定三级镜子和精细转向的后光学子系统(AOS)镜子。 OTE与集成的科学仪器模块(ISIM)相结合,以创建称为OTIS(OTE&ISIM)的全光学列车最近在TX的Johnson Space Center的Champer A中经历了低温真空测试。该测试的一个关键结果是验证PMSA和SMA执行器中是否存在足够的运动,以将它们与飞行条件下的AOS / ISIM对齐。使用摄影测量测量PMSA和SMA的对准状态,并使用经典HARTMANN测试的变型光学地进行交叉检查。在“传球半”(Paah)配置中,CasseGrain聚焦附近的光纤源通过全光学系传播光线,PMSA上的小倾斜在科学仪器探测器上创建了一系列斑点,模仿了效果哈特曼面具。测量和建模的光斑阵列的比较提供了SMA的对准状态和主镜的全球倾斜。本文将讨论使用Hartmann方法测量OTI的对准状态的方法,测试和分析,并验证主镜像可以在轨道上成功对齐以满足性能要求。

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