Power System Concepts for the Lunar Outpost: A Review of the Power Generation, Energy Storage, Power Management and Distribution (PMAD) System Requirements and Potential Technologies for Development of the Lunar Outpost
Abstract
This paper will review potential power system concepts for the development of the lunar outpost including power generation, energy storage and power management and distribution (PMAD). In particular, the requirements of the initial robotic missions will be discussed and the technologies considered will include cryogenics and regenerative fuel cells (RFC), AC and DC transmission line technology, high voltage and low voltage power transmission, conductor materials of construction and power beaming concepts for transmitting power to difficult to access locations such as at the bottom of craters. Operating conditions, component characteristics, reliability, maintainability, constructability, system safety, technology gaps / risk and adaptability for future lunar missions will be discussed for the technologies considered.
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DC systems are more efficient due to the absence of the skin effect, lower line losses, and no reactive power compensation, while allowing simpler design and construction.
“In general, DC systems are more efficient due to the absence of the skin effect, lower line losses, and no reactive power compensation, while allowing simpler design and construction [8], [11].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Lithium-ion batteries have high specific energy (~150-200 Wh/kg) and energy density (more than 200 Wh/l) compared to other rechargeable batteries.
“Lithium-ion (Li-ion) batteries have high specific energy ( ∼ 150 -200 Wh / kg) and energy density (more than 200 Wh / l) compared to other rechargeable batteries [9], [45], [46].”
From Optimal Sizing and Siting of PV and Battery Based Space Microgrids Near the Moon’s Shackleton Crater (2023) · cites this paper as [46]
In Phase 4, a reliable and autonomous system will be operational, enabling safe, permanent human presence upon the Moon.
“in ''Phase 4'' a reliable and autonomous system will be operational, enabling safe, permanent human presence upon the Moon [8].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Polar regions are attractive for establishing a lunar base with less ESS requirements.
“Hence, polar regions are attractive for establishing a lunar base with less ESS requirements [8].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Starting from Phase 3, the lunar establishment is planned to be self-sufficient for operation.
“Starting from ''Phase 3'', the lunar establishment is planned to be self-sufficient for operation”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Increasing the AC system frequency reduces the size of the capacitors and the power converters, but the transmission line mass increases as the skin effect and inductive reactance are directly proportional to the system frequency.
“Increasing the AC system frequency reduces the size of the capacitors and the power converters, but the transmission line mass increases as the skin effect and the inductive reactance is directly proportional to the system frequency [8].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Li-ion batteries have higher specific energy (~100Wh/kg) and energy density (more than 200Wh/l) along with significant mass advantage and operational capability over a wide range of temperature compared to Ni-H2 batteries.
“Li-ion batteries have higher specific energy (∼100Wh/kg) and energy density (more than 200Wh/l) along with significant mass advantage and operational capability over a wide range of temperature compared to Ni-H 2 batteries [8], [59].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Additional energy and specific infrastructures (like pumps) are required to transport the reactants to the surface.
“However, additional energy and specific infrastructures (like pumps) are required to transport the reactants to the surface [8].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Due to the low conductivity of the lunar regolith, charged clouds of lunar dust move around the surface, necessitating additional protection relays and grounding wells for reliable operation.
“Also, due to the low conductivity of the lunar regolith, charged clouds of lunar dust move around the surface, necessitating additional protection relays and grounding wells for reliable operation [8].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Studies have shown that increasing the system frequency does not significantly reduce the overall system mass.
“Thus, studies have shown that increasing the system frequency does not significantly reduce the overall system mass [8].”
From Space Microgrids for Future Manned Lunar Bases: A Review (2021) · cites this paper as [8]
Cites
Lunar polar topography derived from Clementine stereoimages
Cook, A. C., Watters, T. R., Robinson, M. S., Spudis, P. D., & Bussey, D. B. J. (2000) · Journal of Geophysical Research Atmospheres · doi:10.1029/1999je001083 · Cited by 48 · see citing works
Electric Power System Technology Options for Lunar Surface Missions
Kerslake, T. W. (2013) · NASA Technical Reports Server (NASA) · Cited by 12 · see citing works
Power requirements for the first lunar outpost
Cataldo, R. L., & Bozek, J. M. (1993) · AIP conference proceedings · doi:10.1063/1.43249 · Cited by 5 · see citing works
Power requirements for the first lunar outpost (FLO)
Cataldo, R. L., & Bozek, J. M. (1993) · NASA Technical Reports Server (NASA) · Cited by 3 · see citing works
Issues concerning centralized versus decentralized power deployment
Metcalf, K. J., Harty, R. B., & Robin, J. F. (1991) · NASA Technical Reports Server (NASA) · Cited by 2 · see citing works
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Space Microgrids for Future Manned Lunar Bases: A Review
Saha, D., Bazmohammadi, N., Raya-Armenta, J. M., Bintoudi, A. D., Lashab, A., Vasquez, J. C., & Guerrero, J. M. (2021) · IEEE Open Access Journal of Power and Energy · doi:10.1109/oajpe.2021.3116674 · Cited by 64 · see citing works
Parametric Study of a Lunar Base Power Systems
Kaczmarzyk, M., & Musiał, M. (2021) · Energies · doi:10.3390/en14041141 · Cited by 43 · see citing works
“In 2002 Cohen [57] stated, that the typical concepts of baseline Lunar outposts with a long-term human presence (90 days or more) propose power levels of 12 to 30 kW. Khan et al., 2006 [58] demonstrated a lunar base concept with an 81-kW power requirement, including 43 kW for ISRU mining purposes.”
Optimal Sizing and Siting of PV and Battery Based Space Microgrids Near the Moon’s Shackleton Crater
Saha, D., Bazmohammadi, N., Raya-Armenta, J. M., Bintoudi, A. D., Lashab, A., Vasquez, J. C., & Guerrero, J. M. (2023) · IEEE Access · doi:10.1109/access.2023.3239303 · Cited by 32 · see citing works
“Lithium-ion (Li-ion) batteries have high specific energy (∼150−200 Wh/kg) and energy density (more than 200 Wh/l) compared to other rechargeable batteries [9], [45], [46].”
BackgroundLunar Surface-to-Surface Power Transfer
Kerslake, T. W., & El-Genk, M. S. (2008) · AIP Conference Proceedings · doi:10.1063/1.2845004 · Cited by 20 · see citing works
Characteristic of thermal energy system self-driven by exhausted heat from equipment in lunar base
Zhang, K., Sun, P., Li, S., Spataru, C., Lv, X., & Weng, Y. (2022) · Applied Thermal Engineering · doi:10.1016/j.applthermaleng.2022.118751 · Cited by 18 · see citing works
Saha, A., & Ghassemi, M. (2024) · Aerospace · doi:10.3390/aerospace11080685 · Cited by 8 · see citing works
“These systems are crucial for sustaining a long-term presence on the moon, supporting human activities, enabling research efforts, and powering vital technological activities [1–3].”
Background
- Authors
- Khan, Z.
- Affiliations
- Bechtel (United States) (US)
- Corresponding author
- Khan, Z.
- ORCID
- Khan, Z.
- Venue
- AIP Conference Proceedings
- Publisher
- AIP
- Published
- 2006
- Volume
- 813
- Pages
- 1083-1092
- ISSN
- 0094-243X (ISSN-L)
- OpenAlex
- W2125746888
- Cited by
- 36
- References
- 5
- Citations by year
- 2026: 3 · 2025: 3 · 2024: 8 · 2023: 8 · 2022: 5 · 2021: 4 · 2020: 1 · 2019: 2
- FWCI
- 1.22
- Type
- conference paper
- Language
- en
- Open access
- closed
- Locations
- AIP conference proceedings (publishedVersion)
- NASA STI Repository (National Aeronautics and Space Administration) (submittedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Energy › Energy Engineering and Power Technology › Power Systems and Renewable Energy
- Physical Sciences › Engineering › Aerospace Engineering › Space Exploration and Technology
- Keywords
- lunar base, lunar power systems, electricity generation, energy storage, power distribution management, regenerative fuel cells, cryogenics, high-voltage transmission, conductor materials, power beaming, robotic lunar missions, technological risk, system reliability
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