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Challenges of designing and testing a highly stable sensor platform:Cesic® solves MTG Star Sensor Bracket thermoelastie requirements

机译:设计和测试高度稳定的传感器平台的挑战:Cesic®解决了MTG星型传感器支架热弹性要求

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The Meteosat Third Generation's extreme pointing requirements call for a highly stable bracket for mounting the Star Trackers. HB-Cesic®, a chopped fibre reinforced silicon carbide, was selected as a base material for the sensor bracket. The high thermal conductivity and low thermal expansion of HB-Cesic® were the key properties to fulfil the demanding thermo-elastic pointing requirements of below 1 μrad/K for the Star Trackers mounting interfaces. Dominated by thermoelastie stability requirements, the design and analysis of the Bracket required a multidisciplinary approach with the focus on thermal and thermo-elastic analyses. Dedicated modal and thermal post-processing strategies have been applied in the scope of the light weighting process. The experimental verification of this thermo-elastic stable system has been a challenging task of its own. A thermo-elastic distortion measurement rig was developed with a stability of <0.1 μrad/K in all three rotational degrees of freedom.
机译:Meteosat第三代的极端指向要求要求使用高度稳定的支架来安装星追踪器。短纤维增强的碳化硅HB-Cesic®被选作传感器支架的基础材料。 HB-Cesic®的高导热率和低热膨胀率是满足Star Trackers安装接口满足低于1μrad/ K的热弹性指向要求的关键特性。受热弹性稳定性要求支配,支架的设计和分析需要采用多学科方法,重点是热分析和热弹性分析。专用的模态和热后处理策略已应用于轻量化过程的范围。这种热弹性稳定系统的实验验证本身就是一项艰巨的任务。开发了一种热弹性变形测量装置,在所有三个旋转自由度上的稳定性均<0.1μrad/ K。

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