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多级运载火箭动态级间分离的MonteCarlo仿真

J·柔沙尼安 M·塔利班

J·柔沙尼安, M·塔利班. 多级运载火箭动态级间分离的MonteCarlo仿真[J]. 应用数学和力学, 2008, 29(11): 1279-1292.
引用本文: J·柔沙尼安, M·塔利班. 多级运载火箭动态级间分离的MonteCarlo仿真[J]. 应用数学和力学, 2008, 29(11): 1279-1292.
J. Roshanian, M. Talebi. Monte Carlo Simulation of Stage Separation Dynamic of a Multistage Launch Vehicle[J]. Applied Mathematics and Mechanics, 2008, 29(11): 1279-1292.
Citation: J. Roshanian, M. Talebi. Monte Carlo Simulation of Stage Separation Dynamic of a Multistage Launch Vehicle[J]. Applied Mathematics and Mechanics, 2008, 29(11): 1279-1292.

多级运载火箭动态级间分离的MonteCarlo仿真

详细信息
  • 中图分类号: V421.7;O242.2

Monte Carlo Simulation of Stage Separation Dynamic of a Multistage Launch Vehicle

  • 摘要: 提出了研究多级运载火箭级间冷、热分离的计算公式.利用Monte Carlo仿真,考虑箭体分离时,采用远离正常设计值的参数去评估分离失败的风险.分析了各种扰动,如动态不平衡,剩余推力,分离机构引起的分离扰动,以及冷、热分离未对准的影响,得到分离箭体不会发生碰撞的条件.结果表明,当前设计满足分离要求.
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出版历程
  • 收稿日期:  2007-06-19
  • 修回日期:  2008-08-07
  • 刊出日期:  2008-11-15

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