航天器工程2019，Vol.28Issue(3)：52-55,4.DOI:10.3969/j.issn.1673﹣8748.2019.03.009
航天器蜂窝夹层板对称热变形分析及试验验证
Symmetrical Thermal Deformation Analysis and Test Verification for Satellite Honeycomb Sandwich Plate
MA Chao 1CHEN Jing 1WANG Zhiguo 1GU Zhiyue 1ZHANG Rubian 1MAO Min1
作者信息
- 1. Shanghai Institute of Satellite Engineering,Shanghai 201109,China
- 折叠
摘要
Abstract
The thermal deformation of satellite honeycomb sandwich plate in plane temperature field is analyzed in this paper,the control equation and series solution in consideration of honey﹣comb core’s transversal deformation is also given.The thermal deformation test was designed;the change of optical axis pointing was adopted by digital close﹣up photogrammetry.The theoreti﹣cal results are in good agreement with the experimental results,which indicates that the theoreti﹣cal model can be used to prefabricate the thermal deformation.Under typical high and low tem﹣perature working conditions,the optical axis pointing error caused by symmetrical thermal de﹣formation of aluminum honeycomb sandwich plate is about 20″.The relatively sparse and short honeycomb core can reduce the influence of thermal deformation.关键词
航天器/蜂窝夹层板/对称热变形/光轴指向Key words
spacecraft/honeycomb sandwich plate/symmetrical thermal deformation/optical axis pointing分类
通用工业技术引用本文复制引用
MA Chao,CHEN Jing,WANG Zhiguo,GU Zhiyue,ZHANG Rubian,MAO Min..航天器蜂窝夹层板对称热变形分析及试验验证[J].航天器工程,2019,28(3):52-55,4.
