Novel structural design method of special-shaped lightweight aluminum mirror for space spectrometer

Dazhou Xiao, Like Wang, Chao Han, Yuxiang Liu, Ruicong He, Qian Cao
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Abstract

The continuous improvement in the performance and stability of space spectrometers, which include spectral range, spectral resolution, and spectral distortion, makes optical system increasingly complex, which means more optical components are required. However, space missions have strict restrictions on volume and weight. Therefore, light and compact design of space spectrometers are required. The aluminum mirror can undertake both optical and bearing functions, which is one of the key technologies to address this challenge and realize the light and compact optical-mechanical system that has broad applications. A novel structure design method for special-shaped lightweight aluminum mirror of space spectrometers is proposed in this study, which includes scheme design, assembly deformation and unloading structure mode analysis, and lightweight design method. The aluminum mirrors of a hyperspectral remote spectrometer is designed by this method to verify the effectiveness of the method. Different load-bearing structures and weight reduction designs are designed for different aluminum mirrors, so that the weight of this high complexity and multi temperature spectrometer is reduced by 50% while the accuracy remains unchanged.
空间光谱仪异形轻量化铝镜结构设计新方法
空间光谱仪在光谱范围、光谱分辨率、光谱畸变等性能和稳定性方面的不断提高,使得光学系统越来越复杂,需要更多的光学元件。然而,太空任务对体积和重量有严格的限制。因此,对空间光谱仪的设计提出了轻量化、紧凑型的要求。铝镜兼具光学和承载功能,是解决这一难题、实现轻量化、紧凑型光机系统的关键技术之一,具有广阔的应用前景。提出了一种新型空间光谱仪异形轻量化铝镜结构设计方法,包括方案设计、装配变形与卸载结构模态分析以及轻量化设计方法。利用该方法设计了一台高光谱遥感光谱仪的铝镜,验证了该方法的有效性。针对不同的铝制反射镜设计了不同的承重结构和减重设计,使这款高复杂性多温度光谱仪的重量减轻了50%,同时精度保持不变。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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