Landing conditions of space capsule have a great effect on impact characteristics. Firstly, the analysis and simulation model of space capsule was established and validated according to an available experimental data. Methods for explicit nonlinear kinetics analysis were used to simulate the landing impact process of space capsule. And the significance effect and the influence disciplines of parameters related to landing conditions on impact characteristics were analyzed by the orthogonal test design. Results demonstrate that the vertical velocity, the pitch angle, the heeling angle and their interactions significantly influence the maximum impact acceleration, while the horizontal velocity and the rolling angle rarely influence it. These conclusions can provide important reference to both the ground tests of landing impact as well as the structural analysis and design.
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张大鹏,雷勇军.返回舱着陆工况对着陆冲击特性的影响[J].国防科技大学学报,2014,36(6):76-81. ZHANG Dapeng, LEI Yongjun. Impact analysis of landing conditions on space capsule’s impact characteristics[J]. Journal of National University of Defense Technology,2014,36(6):76-81.