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Ultra-high-precision reflectors - design concepts, structural optimization and zero-expansion composites

机译:超高精度反射器-设计概念,结构优化和零膨胀复合材料

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摘要

The developing of satellite remote sensing technology demands high precision reflectors. This paper is devoted to the development of an ultra-high precision reflector, including the structural design and optimization, and even a kind of zero-expansion composite. A novel parabolic reflector without the traditional back surface is designed, simulated and analyzed. The relationships of some key parameters(surface error and weight) with other structural parameters are obtained. As the Kevlar fabric has negative CTE (Coefficient of Thermal Expansion) and CFRP has positive CTE, a Kevlar fabric-assisted carbon fiber composite is suggested. This composite exhibits the advantage of zero-expansion in 2D plane. Further, this zero-expansion laminate has been successfully manufactured. Finally, based on the design and analysis of the zero-expansion composite with CFRP and Kevlar fabric, an ultrahigh-precision reflector is successfully designed. The results of finite element method (FEM) show that the thermal distortion of the reflector meets the requirements of remote satellite, whose working radio frequency (RF) is 600 GHz.
机译:卫星遥感技术的发展需要高精度的反射镜。本文致力于超高精度反射镜的开发,包括结构设计和优化,甚至是一种零膨胀复合材料。设计,模拟和分析了一种新型的抛物面反射镜,它没有传统的背面。得到了一些关键参数(表面误差和重量)与其他结构参数之间的关系。由于Kevlar织物的CTE(热膨胀系数)为负,而CFRP的CTE为正,因此建议使用Kevlar织物辅助的碳纤维复合材料。这种复合材料在二维平面中具有零膨胀的优势。此外,已经成功地制造了这种零膨胀层压材料。最后,基于CFRP和芳纶纤维零膨胀复合材料的设计与分析,成功设计了超高精度反射器。有限元法(FEM)的结果表明,反射器的热变形符合工作频率为600 GHz的远程卫星的要求。

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