A computational model for assessing high-velocity debris impact in space applications
作者: M. BerghV. Garcia
作者单位: 1Swedish Defence Research Agency (FOI)
2OHB Sweden
刊名: Shock Waves, 2017, Vol.27 (4), pp.675-684
来源数据库: Springer Nature Journal
DOI: 10.1007/s00193-017-0709-9
关键词: Hypervelocity impactSpace debrisShock wavesHydrazine initiationMolecular dynamicsReaxFF
原始语种摘要: Man-made space debris is dominating the background meteorite environment with a growing debris population leading to increased collision risks for satellites, especially in the low Earth orbit and geostationary orbit protected environments. Here we present a computational model for estimating the effect of hypervelocity impact from debris particles on non-shielded propellant and pressurant tanks. Eulerian hydrocode simulation is utilised to model firstly penetration and shock wave formation in the propellant and secondly subsequent detonation wave propagation and interaction with the tank wall. Furthermore, reactive molecular dynamics is used to estimate the risk of detonation in a liquid hydrazine layer. We present simulations of a 3.5 mm aluminium spherical debris particle at a velocity...
全文获取路径: Springer Nature  (合作)
影响因子:0.604 (2012)

  • debris 岩屑
  • velocity 速度
  • computational 计算的
  • impact 冲击碰撞
  • propellant 推进剂
  • detonation 爆震
  • dynamics 动力学
  • orbit 轨道
  • hydrazine 联氨
  • geostationary 对地静止的