Abstract

This study proposes a new way to manufacture large lightweight aspherics for space telescopes using stress mirror polishing (SMP). This technique is well known to allow reaching high quality optical surfaces in a minimum time period, thanks to a spherical full-size polishing tool. To obtain the correct surface's aspheric shape, it is necessary to define precisely the thickness distribution of the mirror to be deformed, according to the manufacturing parameters. We first introduce active optics and stress mirror polishing techniques, and then we describe the process to obtain the appropriate thickness mirror distribution, allowing to generate the required aspheric shape during polishing phase. Shape optimization procedure using PYTHON programing and NASTRAN optimization solver using finite element model (FEM) is developed and discussed in order to assist this process. The main result of this paper is the ability of the shape optimization process to support SMP technique to generate a peculiar aspherical shape from a spherical optical surface thanks to a thickness distribution reshaping. This paper is primarily focused on a theoretical framework with numerical simulations as the first step before the manufacturing of a demonstrator. This two-step approach was successfully used for previous projects.

Highlights

  • Stress Mirror Polishing (SMP) is a manufacturing method allowing to obtain the required shape of optical surfaces using deformation and elasticity properties of materials

  • We investigated the possibility to produce such a lightweight aspheric primary mirror for space telescopes using classical elasticity theory combined with new tools

  • An algorithm has been developed allowing to optimize the deformation obtained, using data provided by Finite Element Model (FEM) outputs which has been implemented in Python language

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Summary

Introduction

Stress Mirror Polishing (SMP) is a manufacturing method allowing to obtain the required shape of optical surfaces using deformation and elasticity properties of materials. SMP techniques have a significant benefit for the manufacturing of large lightweight aspheric primary mirrors for space telescopes, especially as they can be applied on a thin shell mirror and combined with an active support [7] or a rigid assembly using a sandwich structure with two facesheets and a Carbon Fiber Reinforced Composite (CFRC) honeycomb [8] This could be perfectly suited for manufacturing of ultra high surface quality primary mirrors, as the ones foreseen in future high-contrast imaging missions for exoplanets detection and characterization, or to have a gain in term of manufacturing time for more classical mirrors. An algorithm has been developed allowing to optimize the deformation obtained, using data provided by Finite Element Model (FEM) outputs which has been implemented in Python language

Definition
Active Optics and 3rd order spherical aberration generation
Shape optimization and Pure 3rd-order spherical aberration
Problem Formulation
Shape optimization algorithm
Initial design
Objective function Constraints
Results and Discussions
Conclusions
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