Design of rectangular space mirror and its support structure

LI Zhi-lai; XU Hong

doi:10.3788/OPE.20111905.1039

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Design of rectangular space mirror and its support structure

Article | 更新时间：2020-08-12

- Design of rectangular space mirror and its support structure
- Optics and Precision Engineering Vol. 19, Issue 5, Pages: 1039-1047(2011)
- 作者机构：
  
  中国科学院长春光学精密机械与物理研究所,吉林长春 130033
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20111905.1039
  CLC： V475.3;TH703
- Received：02 September 2010，
  
  Revised：28 September 2010，
  
  Published Online：26 May 2011，
  
  Published：26 May 2011
- 稿件说明：
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李志来, 徐宏. 长条形空间反射镜及其支撑结构设计[J]. 光学精密工程, 2011,19(5): 1039-1047

LI Zhi-lai, XU Hong. Design of rectangular space mirror and its support structure[J]. Editorial Office of Optics and Precision Engineering, 2011,19(5): 1039-1047
李志来, 徐宏. 长条形空间反射镜及其支撑结构设计[J]. 光学精密工程, 2011,19(5): 1039-1047 DOI： 10.3788/OPE.20111905.1039.

LI Zhi-lai, XU Hong. Design of rectangular space mirror and its support structure[J]. Editorial Office of Optics and Precision Engineering, 2011,19(5): 1039-1047 DOI： 10.3788/OPE.20111905.1039.

摘要

提出了一种空间反射镜柔性支撑结构

以满足反射镜在重力和温变载荷下对较高面形精度的要求。根据光学设计指标要求确定了反射镜的结构形式

根据该结构形式设计了柔性支撑结构

并利用有限元分析软件对反射镜组件进行了分析和结构优化。分析结果表明

反射镜组件的一阶固有频率达到179 Hz

在

3轴方向1

重力作用下镜面面形误差RMS值分别达到5.06

4.43

7.59 nm;在3个方向1

重力和4 ℃温升耦合作用下

镜面综合面形误差RMS值分别达到6.08

6.32

8.08 nm。实验室静态检测结果表明

反射镜在4℃温变条件下能够保证像质

力学试验结果与理论分析基本吻合;经过力学与热真空环境试验后

反射镜面形变化不明显。分析及试验结果表明

反射镜及其支撑结构设计合理

能够满足空间应用要求。

Abstract

A flexible support structure was proposed to keep the higher surface figure accuracy of space mirrors under gravity and uniform temperature change load cases. According to the optical design requirements

the structural form of a mirror was determined

and then a flexible support structure of the primary mirror was designed. By adopting finite element analysis software

the mirror component was analyzed and its structure was optimized. Analysis results show that the first order natural frequency of the mirror component is 179 Hz

and the surface figure accuracy RMS of the mirror reaches 5.06

4.43 and 7.59 nm when gravity load is applied in the directions of

and

axes

respectively. Furthermore

the integrated surface figure accuracy RMS of the mirror reaches 6.08

6.32 and 8.08 nm respectively under the load cases of gravity in three directions coupled with uniform temperature rise of 4 ℃. Laboratory test results indicate that the mirror can offer a good image quality under the condition of 4 ℃ uniform temperature change

and the mechanical test results are consistent with that of the theoretical analysis. The change of the surface figure accuracy is not obvious after dynamic and thermal vacuum tests. Analysis and experimental results demonstrate that designs of the mirror and its support structure are effective

which can meet the requirements of space applications.

关键词

Keywords

references

张科科,阮宁娟,傅丹鹰. 国外空间用三反离轴相机发展分析与思考[J]. 航天返回与遥感, 2008,29(3):63-70. ZHANG K K, RUAN N J, FU D Y. Analysis and consideration of development of overseas space off-axis TMA system camera[J]. Spacecraft Recovery & Remote Sensing, 2008,29(3):63-70. (in Chinese)[2] 鲍赫,李志来. 长条型SiC反射镜轻量化及支撑结构的设计[J]. 光学技术,2008,34(4):593-596. BAO H, LI ZH L. Design of the strip SiC mirror supporting structure and lightweight[J]. Optical Technique, 2008,34(4):593-596.(in Chinese)[3] 王忠素,翟岩,梅贵,等. 空间光学遥感器反射镜柔性支撑的设计[J]. 光学精密工程,2010,18(8):1833-1841. WANG Z S, ZHAI Y, MEI G, et al.. Design of flexible support structure of refector in space remote sensor[J]. Opt. Precision Eng., 2010,18(8):1833-1841. (in Chinese)[4] 张学军. 基于SiC材料的空间相机非球面反射镜结构设计[J]. 红外与激光工程,2007,36(5):577-582. ZHANG X J. Space telescope aspherical mirror structure design based on SiC material [J]. Infrared and Laser Engineering, 2007,36(5):577-582. (in Chinese)[5] 李志来. 长焦距大视场光学系统的光机结构设计[J]. 光学精密工程,2008,16(12):2485-2490. LI ZH L. Optical and mechanical design for long focal length and wide-field optical system [J]. Opt. Precision Eng., 2008,16(12):2485-2490. (in Chinese)[6] YODER P. Opto-mechanical Systems Design [M]. 2nd ed. New York: Marcel Dekker Inc., 1993.[7] FRIEDMAN E. Photonics Rules of Thumb [M]. New York:McGraw Hill, 2003.[8] VUKOBRATOVICH D. Introduction to Optomechanical Design [M]. SPIE Short Course SC014, 2003.[9] 范镝. 反应烧结碳化硅平面反射镜的光学加工[J]. 光学技术,2003,29(6):667-668. FAN D. Optical surfacing of flat reaction-burned silicon carbide mirror[J]. Optical Technique, 2003,29(6):667-668.(in Chinese)[10] 闫勇. 新型轻质大口径空间反射镜支撑设计[J]. 光学精密工程,2008,16(8):1533-1539. YAN Y. Design of new type spaceborne lightweighted primary mirror support[J]. Opt. Precision Eng., 2008,16(8):1533-1539. (in Chinese)[11] 郭疆. 大口径空间遥感相机主反射镜支撑设计[J]. 光学精密工程,2008,16(9):1642-1647. GUO J. Design of support for primary mirror of space remote sensing camera[J]. Opt. Precision Eng., 2008,16(9):1642-1647. (in Chinese)[12] 吴清文. 空间相机中反射镜及其支撑方案设计与分析方法[J]. 光学技术, 2004, 30(2): 153-156. WU Q W. Design and analysis for primary mirror and its support of space camera[J]. Optical Technique, 2004,30(2):153-156.(in Chinese)[13] 孙宝玉. 空间光学遥感器柔性支撑结构设计[J]. 哈尔滨工业大学学报,2009,41(7):642-645. SUN B Y. Design of flexible supporting structure for optical space remote sensor [J]. Journal of Harbin Institute of Technology, 2009,41(7):642-645.(in Chinese)

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Related Institution

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