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Modeling and structural analysis of honeycomb structure mirror
Yeping Li
2012-09-13
Source PublicationModern Technologies in Space- and Ground-based Telescopes and Instrumentation II
Volume8450
Issue8450
PagesVol.8450 4K-1-6
Conference Date2012-7-1
Conference PlaceAmsterdam, Netherlands
Funding OrganizationThe International Society for Optical Engineering
PublisherSPIE
Abstract
In development of large-scale astronomical telescopes, some promising new technology and method such as honeycomb structure mirrors and silicon carbide mirrors are applied for primary mirrors. Especially in space telescopes, the mirror lightweight design is becoming the key technology and honeycomb structure mirrors are normally required
more and more to reduce the cost and increase the feasibility of the telescopes system. In this paper, a parameter FEA model of a two meters honeycomb structure mirror has been built, by using the engineering analysis software ANSYS. Through this model, the structural analysis, thermal deformation analysis and the simulation active correction of loworder frequency aberration by the finite element method have been presented.
KeywordLarge Telescope Honeycomb Mirror Fea Model Active Optics Structural Analysis Thermal Deformation
Subject Area天文镜面(材料、加工、检测) ; 有限元分析
Document Type会议论文
Identifierhttp://ir.niaot.ac.cn/handle/114a32/693
Collection会议论文
Recommended Citation
GB/T 7714
Yeping Li. Modeling and structural analysis of honeycomb structure mirror[C]:SPIE,2012:Vol.8450 4K-1-6.
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