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Analysis of landing site attributes for future missions targeting the rim of the lunar South Pole Aitken basin

机译:针对着陆点南极艾特肯盆地边缘的未来任务的着陆点属性分析

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摘要

For the South polar lunar region between - 85 and - 90° Latitude an updated analyses of the solar illumination and ground station visibility conditions has been performed in the frame of a feasibility study for an ESA Lunar Lander mission. The analyses are based on the refined lunar digital elevation model provided by the Japanese Kaguya/Selene mission, originating from its LASER altimeter instrument For the South polar region maps of integral solar illumination are presented for a mission epoch in 2016. The analysis modelling was validated with the help of a Kaguya High Definition video. The solar illumination is driving for the power subsystems of any robotic lander craft or manned lunar outpost, in case they rely on conventional photovoltaic power generation with battery buffering of shadowed periods. In addition the visibility of the terrain from a terrestrial ESA ground station was analysed. The results are presented as an integral ground contact duration map, being crucial for the operations of any lunar outpost. Considering these two quality criteria, several possible landing sites for a future lunar mission have been pre-selected. For these sites a detailed analysis of quasi-continuous illumination conditions is presented. This includes magnified maps of the pre-selected areas, showing any location's longest illumination intervals that are allowed to be interrupted by shadows with limited duration only. As a final quality criterion, the terrain topology has been analysed for its impact on the landing trajectory. From a tradeoff between the three quality criteria the connecting ridge between the Shackleton and the de Gerlache was determined to provide the most favourable landing site quality. This site is located at 89°28' South, 136°40' West, and 1947 m altitude, and features and integral illumination of 85.7%. With battery energy to sustain shadows of 120 h, total mission duration of 9.37 sidereal months can be guaranteed.
机译:对于纬度介于-85和-90°之间的南极月球区域,在ESA月球着陆器任务的可行性研究框架内,对太阳光照和地面站的能见度条件进行了更新分析。这些分析基于日本Kaguya / Selene任务提供的精确的月球数字高程模型,该模型源自其LASER高度计仪器。2016年,为任务任务时期的南极地区提供了整体太阳照亮地图。分析模型得到了验证在Kaguya高清视频的帮助下。万一它们依赖于传统的光伏发电技术以及遮蔽期的电池缓冲,那么太阳能照明将驱动任何机器人着陆器或载人登月哨所的电源子系统。此外,还分析了地面ESA地面站的地形可见性。结果以完整的地面接触持续时间图表示,这对于任何月球前哨基地的运作都是至关重要的。考虑到这两个质量标准,已经为未来的登月任务选择了几个可能的着陆点。对于这些站点,将对准连续照明条件进行详细分析。这包括预选区域的放大地图,显示了任何位置的最长照明间隔,这些间隔只能被持续时间有限的阴影打断。作为最终质量标准,已经分析了地形拓扑对着陆轨迹的影响。通过三个质量标准之间的权衡,确定了沙克尔顿和德格拉什之间的连接脊可提供最有利的着陆点质量。该站点位于南89°28',西136°40'和1947 m的高度,其整体照明度为85.7%。利用电池能量维持120小时的阴影,可以确保9.37静止个月的总任务持续时间。

著录项

  • 来源
    《Acta astronautica》 |2012年第novaadeca期|p.197-215|共19页
  • 作者单位

    OHB-System AC, Germany, Karl-Ferdinand-Braun-Strasse 8, D-28359 Bremen, Bremen, Germany;

    OHB-System AC, Germany, Karl-Ferdinand-Braun-Strasse 8, D-28359 Bremen, Bremen, Germany;

    OHB-System AC, Germany, Karl-Ferdinand-Braun-Strasse 8, D-28359 Bremen, Bremen, Germany;

    OHB-System AC, Germany, Karl-Ferdinand-Braun-Strasse 8, D-28359 Bremen, Bremen, Germany;

    OHB-System AC, Germany, Karl-Ferdinand-Braun-Strasse 8, D-28359 Bremen, Bremen, 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

    moon; south pole; photovoltaic; illumination map; kaguya digital elevation map;

    机译:月亮;南极;光伏照明图神谷数码高程图;

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