Thermal-Mechanical Design of a Baffle

for the Deployable Space Telescope

Master thesis (2019)

Authors

J. Arink Aerospace Engineering

Contributors

Hans Kuiper (mentor)
M.C. Naeije (mentor)
Pieter N. A. M. Visser (graduation committee member)
Henk Cruijssen (graduation committee member)
Faculty
Aerospace Engineering, Aerospace Engineering
Copyright: © 2019 Jan-Willem Arink
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Published Date

11-10-2019

Language

English

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Faculty

Aerospace Engineering

Abstract

Bottom-up thermal-mechanical design and analysis of a deployable baffle, which serves as a deployable thermal control system for the Deployable Space Telescope. Research being conducted on how to create a stable thermal environment for the mirror support structures so that in-orbit thermo-elastic drift budgets will be met, as well as designing and analysing a feasible deployment system.

Files

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