Heat storage and electricity generation in the Moon during the lunar night |
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| Institution: | 1. Universitat Politècnica de Catalunya - BarcelonaTech, Spain;2. Center for System Studies, University of Alabama in Huntsville, USA;3. Institut Supérieur de l''Aéronautique et de l''Espace, SupAero, France;4. Jacobs Technology, NASA Marshall Space Flight Center, USA;5. Schafer Corporation, USA;1. University of Naples Parthenope, Italy;2. University of Naples Federico II, Italy;1. Key Laboratory of Thermo-Fluid Science and Engineering, Ministry of Education, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, PR China;2. Institute of Global Environmental Change, Xi’an Jiaotong University, Xi’an, PR China;3. Department of Earth and Environmental Sciences, University of Michigan, Ann Arbor, Michigan, USA;1. Department of Engineering & Innovation, The Open University, Walton Hall, Milton Keynes, MK7 6AA, UK;2. Department of Physical Sciences, The Open University, Walton Hall, Milton Keynes, MK7 6AA, UK |
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| Abstract: | One of the biggest challenges of the exploration of the Moon is the survival of the crew and the lunar assets during the lunar night. The environmental conditions on the lunar surface and its cycle, with long periods of darkness, make any long mission in need of specific amounts of heat and electricity to be successful. We have analyzed two different systems to produce heat and electricity on the Moon's surface. The first system consists of Thermal Wadis, sources of thermal power that can be used to supply heat to protect the exploration systems from the extreme cold during periods of darkness. Previous results showed that Wadis can supply enough heat to keep lunar devices such as rovers above their minimum operating temperature (approximately 243 K). The second system studied here is the Thermal Energy Storage (TES), which is able to run a heat engine during the lunar night to produce electricity. When the Sun is shining on the Moon's surface, the system can run the engine directly using the solar power and simultaneously heat a thermal mass. This thermal mass is used as a high temperature source to run the heat engine during the night. We present analytical and numerical calculations for the determination of an appropriate thermal mass for the TES system. |
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| Keywords: | Moon Energy System Heat collection Heat storage |
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