首页> 外文会议>Optical systems alignment, tolerancing, and verification IV >Cryogenic performance of a high precision photogrammetry system for verification of the James Webb Space Telescope Integrated Science Instrument Module and associated ground support equipment structural alignment requirements
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Cryogenic performance of a high precision photogrammetry system for verification of the James Webb Space Telescope Integrated Science Instrument Module and associated ground support equipment structural alignment requirements

机译:高精度摄影测量系统的低温性能,可验证詹姆斯·韦伯太空望远镜集成科学仪器模块和相关地面支持设备的结构对准要求

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The James Webb Space Telescope (JWST) is a general astrophysics mission which consists of a 6.6m diameter, segmented, deployable telescope for cryogenic IR space astronomy (~35K). The JWST Observatory architecture includes the Optical Telescope Element and the Integrated Science Instrument Module (ISIM) element that contains four science instruments (SI) including a Guider.rnThe alignment philosophy of ISIM is such that the cryogenic changes in the alignment of the SI interfaces are captured in the ISIM alignment error budget. The Sis are aligned to the structure's coordinate system under ambient, clean room conditions using laser tracker and theodolite metrology. The ISIM structure is thermally cycled and temperature-induced structural changes are concurrently measured with a photogrammetry metrology system to ensure they are within requirements.rnWe compare the ISIM photogrammetry system performance to the ISIM metrology requirements and describe the cryogenic data acquired to verify photogrammetry system level requirements, including measurement uncertainty. The ISIM photogrammetry system is the baseline concept for future tests involving the Optical Telescope Element (OTE) and Observatory level testing at Johnson Space Flight Center.
机译:詹姆斯·韦伯太空望远镜(JWST)是一项常规的天体物理学任务,由直径6.6m的分段可展开望远镜组成,用于低温红外空间天文学(〜35K)。 JWST天文台的体系结构包括光学望远镜元件和集成科学仪器模块(ISIM)元件,其中包含四个包括导引器的科学仪器(SI)。ISIM的对准原理是,SI接口对准中的低温变化是在ISIM对齐错误预算中捕获。使用激光跟踪仪和经纬仪测量技术,可在环境,洁净室条件下将Sis对准结构的坐标系。 ISIM结构经过热循环,并使用摄影测量系统同时测量温度引起的结构变化,以确保它们在要求之内。我们将ISIM摄影测量系统的性能与ISIM计量要求进行比较,并描述所获得的低温数据以验证摄影测量系统的水平要求,包括测量不确定度。 ISIM摄影测量系统是未来测试的基本概念,涉及在约翰逊太空飞行中心进行的光学望远镜元件(OTE)和天文台水平测试。

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