Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge

The lunar polar regions are key areas for future exploration due to the long-term continuous illumination and persistently shadowed regions that can cold trap abundant water and other volatiles. However, the complex terrain, dynamic lighting, and solar wind-induced electric-field environment present...

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Published in:Aerospace
Main Authors: Hong Gan, Chengxuan Zhao, Guangfei Wei, Xiongyao Li, Guojun Xia, Xiao Zhang, Jingjing Shi
Format: Text
Language:English
Published: Multidisciplinary Digital Publishing Institute 2023
Subjects:
Online Access:https://doi.org/10.3390/aerospace10070598
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spelling ftmdpi:oai:mdpi.com:/2226-4310/10/7/598/ 2023-08-20T04:09:52+02:00 Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge Hong Gan Chengxuan Zhao Guangfei Wei Xiongyao Li Guojun Xia Xiao Zhang Jingjing Shi 2023-06-30 application/pdf https://doi.org/10.3390/aerospace10070598 EN eng Multidisciplinary Digital Publishing Institute Astronautics & Space Science https://dx.doi.org/10.3390/aerospace10070598 https://creativecommons.org/licenses/by/4.0/ Aerospace; Volume 10; Issue 7; Pages: 598 lunar south pole illumination condition electric-field environment Chang’E-7 lunar rover Text 2023 ftmdpi https://doi.org/10.3390/aerospace10070598 2023-08-01T10:41:28Z The lunar polar regions are key areas for future exploration due to the long-term continuous illumination and persistently shadowed regions that can cold trap abundant water and other volatiles. However, the complex terrain, dynamic lighting, and solar wind-induced electric-field environment present multiple challenges for polar investigation and sampling missions. China’s Chang’E-7 (CE-7) will explore the Moon’s south polar region in 2026. One of the scientific goals is to drill samples in a wide area with a rover for in situ analysis. This study analyzes the engineering constraints of the polar illumination condition, slopes, and electric field for landing and sampling-site selection. Then, we create a 3D model of CE-7’s lunar rover in three operating environments by employing the Spacecraft Plasma Interaction Software, with the rover sampling (i) on a flat surface, (ii) in a shadow, and (iii) near a meter-scale crater under different solar altitude angles. The results show that the rover can be charged to different potentials under the combined effects of solar wind incident angles and surrounding terrains. We find that a favorable traversing and/or sampling site of the rover for future polar exploration is in the upwind direction of a bulge (positively elevated terrains, such as the lander or boulders) or crater, which will cause a minimum charging effect on the rover. Our results have important implications for minimizing the risk of charging effects and guiding the lunar polar region exploration. Text South pole MDPI Open Access Publishing South Pole Aerospace 10 7 598
institution Open Polar
collection MDPI Open Access Publishing
op_collection_id ftmdpi
language English
topic lunar south pole
illumination condition
electric-field environment
Chang’E-7
lunar rover
spellingShingle lunar south pole
illumination condition
electric-field environment
Chang’E-7
lunar rover
Hong Gan
Chengxuan Zhao
Guangfei Wei
Xiongyao Li
Guojun Xia
Xiao Zhang
Jingjing Shi
Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge
topic_facet lunar south pole
illumination condition
electric-field environment
Chang’E-7
lunar rover
description The lunar polar regions are key areas for future exploration due to the long-term continuous illumination and persistently shadowed regions that can cold trap abundant water and other volatiles. However, the complex terrain, dynamic lighting, and solar wind-induced electric-field environment present multiple challenges for polar investigation and sampling missions. China’s Chang’E-7 (CE-7) will explore the Moon’s south polar region in 2026. One of the scientific goals is to drill samples in a wide area with a rover for in situ analysis. This study analyzes the engineering constraints of the polar illumination condition, slopes, and electric field for landing and sampling-site selection. Then, we create a 3D model of CE-7’s lunar rover in three operating environments by employing the Spacecraft Plasma Interaction Software, with the rover sampling (i) on a flat surface, (ii) in a shadow, and (iii) near a meter-scale crater under different solar altitude angles. The results show that the rover can be charged to different potentials under the combined effects of solar wind incident angles and surrounding terrains. We find that a favorable traversing and/or sampling site of the rover for future polar exploration is in the upwind direction of a bulge (positively elevated terrains, such as the lander or boulders) or crater, which will cause a minimum charging effect on the rover. Our results have important implications for minimizing the risk of charging effects and guiding the lunar polar region exploration.
format Text
author Hong Gan
Chengxuan Zhao
Guangfei Wei
Xiongyao Li
Guojun Xia
Xiao Zhang
Jingjing Shi
author_facet Hong Gan
Chengxuan Zhao
Guangfei Wei
Xiongyao Li
Guojun Xia
Xiao Zhang
Jingjing Shi
author_sort Hong Gan
title Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge
title_short Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge
title_full Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge
title_fullStr Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge
title_full_unstemmed Numerical Simulation of the Lunar Polar Environment: Implications for Rover Exploration Challenge
title_sort numerical simulation of the lunar polar environment: implications for rover exploration challenge
publisher Multidisciplinary Digital Publishing Institute
publishDate 2023
url https://doi.org/10.3390/aerospace10070598
geographic South Pole
geographic_facet South Pole
genre South pole
genre_facet South pole
op_source Aerospace; Volume 10; Issue 7; Pages: 598
op_relation Astronautics & Space Science
https://dx.doi.org/10.3390/aerospace10070598
op_rights https://creativecommons.org/licenses/by/4.0/
op_doi https://doi.org/10.3390/aerospace10070598
container_title Aerospace
container_volume 10
container_issue 7
container_start_page 598
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