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Target selection and comparison of mission design for space debris removal by DLR's advanced study group

机译:DLR高级研究小组的目标选择和任务设计的空间碎片清除比较

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摘要

Space debris is a growing problem. Models show that the Kessler syndrome, the exponential growth of debris due to collisions, has become unavoidable unless an active debris removal program is initiated. The debris population in LEO with inclination between 60° and 95° is considered as the most critical zone. In order to stabilize the debris population in orbit, especially in LEO, 5 to 10 objects will need to be removed every year. The unique circumstances of such a mission could require that several objects are removed with a single launch. This will require a mission to rendezvous with a multitude of objects orbiting on different altitudes, inclinations and planes. Removal models have assumed that the top priority targets will be removed first. However this will lead to a suboptimal mission design and increase the △V-budget. Since there is a multitude of targets to choose from, the targets can be selected for an optimal mission design. In order to select a group of targets for a removal mission the orbital parameters and political constraints should also be taken into account. Within this paper a number of the target selection criteria are presented. The possible mission targets and their order of retrieval is dependent on the mission architecture. A comparison between several global mission architectures is given. Under consideration are 3 global missions of which a number of parameters are varied. The first mission launches multiple separate deorbit kits. The second launches a mother craft with deorbit kits. The third launches an orbital tug which pulls the debris in a lower orbit, after which a deorbit kit performs the final deorbit burn. A RoM mass and cost comparison is presented. The research described in this paper has been conducted as part of an active debris removal study by the Advanced Study Group (ASG). The ASG is an interdisciplinary student group working at the DLR, analyzing existing technologies and developing new ideas into preliminary concepts.
机译:空间碎片是一个日益严重的问题。模型显示,除非启动主动的碎片清除程序,否则由于碰撞导致的碎片呈指数增长的凯斯勒综合症已不可避免。 LEO中的倾斜度在60°至95°之间的碎片群被认为是最关键的区域。为了稳定轨道上的碎片数量,特别是在LEO中,每年需要清除5至10个物体。此类任务的独特情况可能要求一次发射就将多个物体移除。这将需要执行任务,使在不同高度,倾斜度和平面上绕行的许多物体会合。删除模型假设将优先删除最高优先级的目标。但是,这将导致任务设计欠佳,并增加△V预算。由于有许多目标可供选择,因此可以为最佳任务设计选择目标。为了为清除任务选择一组目标,还应考虑轨道参数和政治限制。在本文中,提出了许多目标选择标准。可能的任务目标及其检索顺序取决于任务体系结构。给出了几种全球任务架构之间的比较。正在考虑3个全球任务,其中的许多参数都有所不同。第一个任务是发射多个独立的脱轨套件。第二次发射带有脱轨套件的母舰。第三次发射升空轨道的拖船,将碎片拉到较低的轨道上,此后,脱轨套件执行最后的脱轨燃烧。提出了RoM质量和成本的比较。本文所述的研究已作为高级研究小组(ASG)开展的主动清除碎片研究的一部分。 ASG是DLR的跨学科学生团体,负责分析现有技术并将新的想法发展为初步概念。

著录项

  • 来源
    《Acta astronautica》 |2014年第sepaaocta期|241-248|共8页
  • 作者单位

    Deutsches Zentrum fuer Luft- und Raumfahrt e.V. (DLR), Germany,Delft University of Technology (TU Delft), Netherlands;

    Deutsches Zentrum fuer Luft- und Raumfahrt e.V. (DLR), Germany / OHB System AG, Germany;

    Deutsches Zentrum fuer Luft- und Raumfahrt e.V. (DLR), Germany,Delft University of Technology (TU Delft), Netherlands;

    Deutsches Zentrum fuer Luft- und Raumfahrt e.V. (DLR), Germany / Instituto Superior Ticnico Lisboa, Portugal;

    Deutsches Zentrum fuer Luft- und Raumfahrt e.V. (DLR), Germany;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Space debris; Active space debris removal; Mission design; Target selection; Cost estimation; Mission analysis;

    机译:空间碎片;主动清除空间碎片;任务设计;目标选择;费用估算;任务分析;

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