Thermal–Structural Coupled Analysis and Design of a Reentry Capsule with Ablative Thermal Protection Systems
Author:
Funder
Ministry of Science and ICT, South Korea
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42405-024-00789-3.pdf
Reference33 articles.
1. Mathews RN, Shafeeque AP (2015) Hypersonic flow analysis on an atmospheric re-entry module. Int J of Eng Res and Gen Sci 3:991–1001
2. Le VT, San HN, Goo NS (2021) Advanced sandwich structures for thermal protection systems in hypersonic vehicles: a review. Compos B Eng 226:109301. https://doi.org/10.1016/j.compositesb.2021.109301
3. Uyanna O, Najafi H (2020) Thermal protection systems for space vehicles: a review on technology development, current challenges and future prospects. Acta Astronaut 176:341–356. https://doi.org/10.1016/j.actaastro.2020.06.047
4. Kato S, Matsuda S, Shimada N, Sakai S, Okuyama K, Szasz B, Shimoda T (2019) One-dimensional ablation analysis of lightweight CFRP ablators with coking. Trans Jpn Soc Aeronaut Space Sci Aerosp Technol Japan 17:461–470. https://doi.org/10.2322/tastj.17.461
5. Hasan MZ (2022) Thermal response and surface recession of a carbon-phenolic charring heatshield of spacecraft: numerical simulation and validation. J Space Saf Eng 9:298–318. https://doi.org/10.1016/j.jsse.2022.03.002
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