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LSST Camera Heat Requirements using CFD and Thermal SeeingModeling

机译:使用CFD和热导的LSST相机热量需求 r n建模

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The LSST camera is located above the LSST primary/tertiary mirror and in front of the secondary mirror in the shadow of its central obscuration. Due to this position within the optical path, heat released from the camera has a potential impact on the seeing degradation that is larger than traditionally estimated for Cassegrain or Nasmyth telescope configurations. This paper presents the results of thermal seeing modeling combined with Computational Fluid Dynamics (CFD) analyzes to define the thermal requirements on the LSST camera.rnCamera power output fluxes are applied to the CFD model as boundary conditions to calculate the steady-state temperature distribution on the camera and the air inside the enclosure. Using a previously presented post-processing analysis to calculate the optical seeing based on the mechanical turbulence and temperature variations along the optical path, the optical performance resulting from the seeing is determined. The CFD simulations are repeated for different wind speeds and orientations to identify the worst case scenario and generate an estimate of seeing contribution as a function of camera-air temperature difference. Finally, after comparing with the corresponding error budget term, a maximum allowable temperature for the camera is selected.
机译:LSST摄像机位于LSST主/三级镜的上方,在副镜的中央暗影的阴影下。由于光路中的此位置,从相机释放的热量对视力下降的潜在影响大于对卡塞格林或纳斯米斯望远镜配置的传统估计。本文介绍了热导建模的结果,并结合计算流体动力学(CFD)分析来定义LSST摄像机的热需求.rn将摄像机功率输出通量作为边界条件应用于CFD模型,以计算稳态温度分布。摄像机和外壳内的空气。使用先前提出的后处理分析来基于机械湍流和沿光路的温度变化来计算光学可见性,从而确定由可见性产生的光学性能。针对不同的风速和风向重复进行CFD模拟,以识别最坏的情况,并根据相机-空气温度差生成视线贡献的估计值。最后,在与相应的误差预算项进行比较之后,选择摄像机的最高允许温度。

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