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A METHOD AND A TOOL FOR ASSESSING IN-ORBIT DEBRIS-RELATED RISK FOR SPACE SYSTEMS

机译:一种用于评估空间系统的轨道碎片相关风险的方法和工具

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This paper addresses a methodology taking spacedebris- related risk for Low, Medium and Geostationary Earth Orbit space missions into account, and aims at assessing the collision risk not only as a physical threat supported by a physical spacecraft, but as a hazardous effect on the space system mission. The goal is to develop a tool exploiting such physical simulation results (i.e. effects of sustainable impacts on the spacecraft in case of small debris, cost of the spacecraft avoidance manoeuvres in case of large debris) in a given debris scenario, to compute the repercussion of these effects on the space mission, and to perform comparisons between possible debris scenarios. This work is part of the P2-ROTECT (Prediction, Protection & Reduction of OrbiTal Exposure to Collision Threats) project, initiated in March 2011.
机译:本文涉及一种方法论为低,中和地球地球轨道轨道空间任务考虑了空间相关风险,并旨在评估碰撞风险,不仅是物理航天器支持的身体威胁,而且对空间的危险作用制度使命。目标是开发一种利用这种物理仿真结果的工具(即,在小型碎片的情况下,在小碎片的情况下,在给定的碎片场景中,航天器避免演习的成本,用于计算反应的碎片这些对空间任务的影响,并在可能的碎片场景之间进行比较。这项工作是2011年3月发起的P2-Rotoct(预测,保护和碰撞威胁的预测,保护和减少)项目的一部分。

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