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Optimization Design of Radiation Vault in Jupiter Orbiting Mission

机译:木星轨道轨道轨道辐射拱顶优化设计

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摘要

In Jupiter missions, one significant challenge is the harsh environment. The radiation in Jovian orbit is much higher than that in earth bf vicinity in terms of intensity and energy level. In spacecraft (S/C) design, key electronics are packaged in an enclosed vault to help them survive through the mission. The preliminary optimization design methods of a radiation vault based on a genetic algorithm (GA) are introduced, including shield structure optimization and layout pattern of electronics optimization. In shield structure optimization, the method is combined with a total ionizing dose (TID) evaluation tool. The goal is to find the optimal multi-layer shield structure so that the TID, after the shielding, is minimal within the threshold of the total mass of the structure. In a 1-year mission with an orbit of $10,,R_{j}imes 25,,R_{j} imes 0^{circ }$ , if the areal density is within 0.5–3 g/cm2, the optimal structure is bilayer or trilayer with high-Z material as an external layer and low-Z material as an internal layer. This structure benefits from the fact that the low-Z material is more effective in shielding energetic protons whereas the high-Z material is more effective in shielding energetic electrons. In the 1-g/cm2 situation, the optimal structure is a 0.829-mm lead layer combined with a 0.158-mm magnesium layer. Comparing with the traditional aluminum shielding structure, about 43.6% of mass can be saved. In layout pattern optimization, this method combines a packing algorithm and a 3-D TID simulation tool. Using this method, an effective design layout of the vault can be found. In this design, all avionics can survive through the mission. In addition, the mass of the vault is low enough that the layout pattern is acceptable in S/C design. As an example, 14 instruments with TID threshold of 50 krad (Si) are packaged in a vault. On the premise that one instrument’s walls are thickened to 3.5-mm aluminum, the total mass of the vault is 68.47 kg. This method is a starting point for the iterative design of the radiation vault and gives principle guidelines for the designers.
机译:在木星任务中,一个重大挑战是恶劣的环境。在强度和能量水平方面,Jovian轨道的辐射远高于地球BF附近的辐射。在航天器(S / C)设计中,关键电子产品包装在封闭的穹顶中,以帮助他们通过任务生存。介绍了基于遗传算法(GA)的辐射拱顶的初步优化设计方法,包括屏蔽结构优化和电子优化布局模式。在屏蔽结构优化中,该方法与总电离剂量(TID)评估工具组合。目标是找到最佳的多层屏蔽结构,使得TID在屏蔽之后,在结构的总质量的阈值内最小。在一个轨道的一个1年的使命<内联公式XMLNS:MML =“http://www.w3.org/1998/math/mathml”xmlns:xlink =“http://www.w3.org/1999/xlink”> $ 10 ,,r_ {j} times 25 ,,r_ {j} times 0 ^ { cir} $ ,如果区域密度在0.5-3克/厘米内 2 ,最佳结构是双层或三层,具有高Z材料作为外层和低Z材料作为内层。这种结构效益于低Z材料在屏蔽能量质子中更有效,而高Z材料在屏蔽能量电子中更有效。在1-g / cm中 2 情况,最佳结构是0.829毫米的引线层与0.158mm镁层合并。与传统的铝屏蔽结构相比,可以节省约43.6%的质量。在布局模式优化中,该方法结合了包装算法和3-D TID仿真工具。使用此方法,可以找到Vault的有效设计布局。在这种设计中,所有航空电子都可以通过使命来生存。此外,拱顶的质量足够低,以至于在S / C设计中可以接受布局图案。例如,具有50克拉德(SI)的TID阈值的14个仪器包装在拱顶中。在一个仪器的墙壁增厚到3.5毫米铝的前提下,拱顶的总质量为68.47千克。该方法是辐射保管库的迭代设计的起点,并为设计者提供了原则。

著录项

  • 来源
    《IEEE Transactions on Nuclear Science》 |2019年第10期|2179-2187|共9页
  • 作者单位

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

    Beijing Institute of Spacecraft System Engineering China Academy of Space Technology Beijing China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Optimization; Jupiter; Layout; Protons; Genetic algorithms; Planetary orbits;

    机译:优化;木星;布局;质子;遗传算法;行星轨道;

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