| Issue |
MATEC Web Conf.
Volume 257, 2019
2018 International Conference on Progress in Mechanical and Aerospace Engineering (PMAE 2018)
|
|
|---|---|---|
| Article Number | 01001 | |
| Number of page(s) | 4 | |
| Section | Aerospace Engineering and Applications | |
| DOI | https://doi.org/10.1051/matecconf/201925701001 | |
| Published online | 16 January 2019 | |
Analysis and Study of Heat Transfer Resistance Inside and Outside the Reentry Capsule
Beijing Institute of Spacecraft System Engineering, Beijing, 100094
According to the heat transfer characteristics inside and outside of the lunar-earth high-speed reentry capsule, a typical calculation model of heat conduction in external thermal protection system(TPS) coupled with internal radiation was established. The thermal properties of thermal resistance inside and outside the reentry capsule were analysed. The effects of thickness of the TPS, surface conditions and atmospheric pressures on the temperature were further explored. The results showed that atmosphere pressure was necessary to be controlled under 10Pa to ensure the safety temperature of the equipment and pipe. Based on the critical pressure, the configuration was optimized. The results provide detailed data for the system design of the lunar exploration, and also provide a reference for the thermal design of the atmospheric reentry spacecraft.
© The Authors, published by EDP Sciences, 2019
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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