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首页> 外文期刊>Canadian Aeronautics and Space Journal >Modelling Satellite Vulnerability to Orbital Debris
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Modelling Satellite Vulnerability to Orbital Debris

机译:卫星对轨道碎片的脆弱性建模

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摘要

Beginning in 1990, the Canadian Space Agency conducted a series of studies to determine the probability of survival of the RADARSAT spacecraft, to be launched in 1995. It was found that the artificial debris environment predicted would pose an unacceptable risk to the vehicle. A review of the methods used in these studies revealed that many of the previous estimates of the probability of critical satellite damage had relied on unnecessarily conservative assumptions. In the current study, a method that applied solid modelling was employed which eliminated the need to use these assumptions. Spacecraft components and shielding were modelled, and then a series of simulated impacts were generated to determine component and overall vulnerability. The impacting particle and the resultant debris were modelled using cones centred on the particle's path. The estimated vulnerability is 12 times less than that predicted in previous studies.
机译:从1990年开始,加拿大航天局进行了一系列研究,以确定将于1995年发射的RADARSAT航天器的生存可能性。发现,预测的人工碎片环境将对飞行器构成无法接受的风险。对这些研究中使用的方法的回顾表明,先前对严重卫星损坏的可能性的许多估计都依赖于不必要的保守假设。在当前的研究中,采用了一种应用实体建模的方法,从而消除了使用这些假设的需要。对航天器的组件和屏蔽进行建模,然后生成一系列模拟的影响以确定组件和整体脆弱性。撞击粒子和产生的碎片是使用以粒子路径为中心的圆锥建模的。估计的漏洞比以前的研究预测的漏洞少12倍。

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