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Open Access

Numerical study on water landing characteristics of a reentry capsule with airbag cushioning under calm water and regular/irregular waves

Jiapeng HANaShiqing WUb,cJiangli LEIb,cWei HUANGb,cHuai XIEb,cYang ZHANGa,c( )
College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
Beijing Institute of Space Mechanics and Electricity, Beijing 100096, China
Laboratory of Aerospace Entry, Descent and Landing Technology, China Aerospace Science and Technology Corporation, Beijing 100094, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

This study presents a Fluid-Structure Interaction (FSI) model to analyze the water landing characteristics of a reentry capsule equipped with airbag cushioning. The model employs the Arbitrary Lagrangian-Eulerian (ALE) method to simulate the capsule’s impact with water, while the control volume method is used to model the airbag cushioning process. Additionally, both regular and irregular heading waves are incorporated to simulate the landing dynamics of the capsule-airbag system under various sea conditions. The developed FSI model is utilized to investigate the effects of initial velocity, attitude angle, and wave phase on the water landing characteristics of the capsule-airbag system under calm water, regular and irregular wave conditions. Key parameters, such as the impact force on the capsule, as well as the pressure, mass flow rate, and stress distribution within the airbags, are analyzed. The insights gained from this study provide valuable guidance for minimizing damage to personnel and equipment during maritime recovery operations.

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Chinese Journal of Aeronautics

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Cite this article:
HAN J, WU S, LEI J, et al. Numerical study on water landing characteristics of a reentry capsule with airbag cushioning under calm water and regular/irregular waves. Chinese Journal of Aeronautics, 2025, 38(10). https://doi.org/10.1016/j.cja.2025.103615

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Received: 11 September 2024
Revised: 11 November 2024
Accepted: 25 November 2024
Published: 06 June 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).