Title: Thermal Modelling for Thermoelastic Analysis
Abstract: A spacecraft is going through different phases of a mission. Each of these phases has its own characteristics in terms of thermal environment. The objectives of these different phases drive the difference in focus of thermoelastic analyses from one phase to the other. The lumped parameter thermal analysis method typically used for spacecraft thermal analysis is summarised. Transient thermal analysis is a common analysis approach for simulating time-varying thermal environments along the orbit around a planet. Special attention is paid to the difference between thermal analysis for thermal control and thermal analysis for thermoelastic.
Publication Year: 2021
Publication Date: 2021-08-31
Language: en
Type: book-chapter
Indexed In: ['crossref']
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