土壤参数对返回舱着陆冲击特性的影响分析

张大鹏;雷勇军;段静波;谢燕;郑健

振动与冲击 ›› 2014, Vol. 33 ›› Issue (7) : 120-125.

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振动与冲击 ›› 2014, Vol. 33 ›› Issue (7) : 120-125.
论文

土壤参数对返回舱着陆冲击特性的影响分析

  • 张大鹏1,雷勇军1,段静波1,谢燕1,郑健2
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Impact Analysis of Soil Parameters on Space Capsule’sImpact Characteristic

  • ZHANG Dapeng1,LEI Yongjun1,DUAN Jingbo1,XIE Yan1,ZHENG Jian2
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摘要

建立合理可靠的土壤模型是返回舱着陆冲击仿真分析的关键问题。利用显式动力有限元软件LS-DYNA模拟了返回舱着陆冲击过程,并采用正交试验设计对土壤模型中主要材料参数对着陆冲击响应特性的影响显著性进行了分析。结果表明:土壤材料体积模量、屈服参数A2对最大加速度、冲击脉宽影响较大,土壤材料屈服参数A0、A1对最大加速度、冲击脉宽的影响较小,各参数的交互效应不显著。这些结论可为返回舱着陆冲击过程的相关试验和返回舱设计分析提供参考。

Abstract

The establishment of scientific finite element mode for soil plays a pivotal role in simulating and analyzing the landing impact of space capsule. The LS-DYNA was used to simulate the landing process of space capsule, and the effect of main parameters in soil mode on impact characteristic was analyzed through orthogonal test. The results demonstrate that bulk modulus and parameter A2 significantly influence the maximum impact acceleration and pulse width, parameter A0 A1 and their interaction are not significant. These conclusions can provide some references to both the study on ground test in the landing process and the structural optimization of space capsule.

关键词

返回舱 / 着陆冲击 / LS-DYNA / 试验设计 / 冲击特性

Key words

space capsule / landing impact / LS-DYNA / test design / impact characteristic

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导出引用
张大鹏;雷勇军;段静波;谢燕;郑健. 土壤参数对返回舱着陆冲击特性的影响分析[J]. 振动与冲击, 2014, 33(7): 120-125
ZHANG Dapeng;LEI Yongjun;DUAN Jingbo;XIE Yan;ZHENG Jian. Impact Analysis of Soil Parameters on Space Capsule’sImpact Characteristic[J]. Journal of Vibration and Shock, 2014, 33(7): 120-125

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