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Designing and testing a highly stable ceramic sensor platform for challenging thermoelastic requirements

机译:设计和测试高度稳定的陶瓷传感器平台,用于具有挑战性的热弹性要求

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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 lμrad/K for the Star Trackers mounting interfaces. Dominated by thermoelastic 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. lμrad/K in all three rotational degrees of freedom.
机译:Meteosat第三代的极端指向要求呼叫高度稳定的支架,用于安装星形跟踪器。 HB-CESIC?,切碎的纤维增强碳化硅作为传感器支架的基材。 HB-Cesic的高导热率和低热膨胀?是满足苛刻的热弹性指向要求的关键特性,对于星形跟踪器安装界面,LOμrad/ k以下。以热弹性稳定性要求为主,支架的设计和分析需要多学科方法,重点是热和热弹性分析。专用的模态和热后处理策略已应用于轻量级过程的范围。这种热弹性稳定系统的实验验证是其自身的具有挑战性的任务。具有稳定性<0的热弹性失真测量钻机。 Lμrad/ k在所有三个旋转自由度中。

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