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Characterisation of potential landing sites for the European Space Agency's Lunar Lander project

机译:欧洲航天局的月球着陆器项目潜在着陆点的特征

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This article describes the characterisation activities of the landing sites currently envisaged for the Lunar Lander mission of the European Space Agency. These sites have been identified in the South Pole Region (-85° to-90° latitude) based on favourable illumination conditions, which make it possible to have a long-duration mission with conventional power and thermal control subsystems, capable of enduring relatively short periods of darkness (in the order of tens of hours), instead of utilising Radioisotope Heating Units. The illumination conditions are simulated at the potential landing sites based on topographic data from the Lunar Orbiter Laser Altimeter (LOLA), using three independent tools. Risk assessment of the identified sites is also being performed through independent studies. Long baseline slopes are assessed based on LOLA, while craters and boulders are detected both visually and using computer tools in Lunar Reconnaissance Orbiter Camera (LROC) images, down to a size of less than 2 m, and size-frequency distributions are generated. Shadow hazards are also assessed via LROC images. The preliminary results show that areas with quasi-continuous illumination of several months exist, but their size is small (few hundred metres); the duration of the illumination period drops quickly to less than one month outside the areas, and some areas present gaps with short illumination periods. Concerning hazard distributions, 50 m slopes are found to be shallow (few degrees) based on LOLA, whereas at the scale of the lander footprint (~5 m) they are mostly dominated by craters, expected to be mature (from geological context) and shallow (~11°). The preliminary conclusion is that the environment at the prospective landing sites is within the capabilities of the Lander design.
机译:本文介绍了目前为欧洲航天局的月球着陆器任务设想的着陆点的表征活动。根据有利的照明条件,在南极地区(纬度为-85°至-90°)确定了这些地点,这使得使用常规电源和热控制子系统可以进行较长时间的任务,并且能够承受相对较短的时间一段黑暗的时间(约数十小时),而不是利用放射性同位素加热单元。使用三个独立的工具,根据月球轨道激光测高仪(LOLA)的地形数据,在潜在的着陆点模拟照明条件。还通过独立研究对确定地点的风险进行了评估。基于LOLA评估较长的基线坡度,同时在月球侦察轨道摄像机(LROC)图像中目测和使用计算机工具检测陨石坑和巨石,直至小于2 m的尺寸,并生成尺寸-频率分布。还可以通过LROC图像评估阴影危害。初步结果表明,存在几个月连续照明的区域,但面积很小(几百米)。照明时间的持续时间迅速下降到区域外不到一个月,并且某些区域的照明时间较短。关于危险性分布,根据LOLA,发现50 m的斜坡是浅的(几度),而在着陆器足迹的范围(〜5 m)上,它们主要由火山口控制,预计将是成熟的(根据地质情况),浅(〜11°)。初步结论是,预期着陆点的环境在Lander设计的能力范围内。

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