TY - GEN
T1 - Multi-Functional Lunar Surface Service Hubs
AU - Thangavelautham, Jekan
AU - Vernekar, Harish
AU - Dinkel, Anna
AU - van der Leeuw, Nathaniel
AU - Torres, Andrea
AU - Muralidharan, Krishna
AU - Asphaug, Erik
AU - Dickinson, Cameron
N1 - Publisher Copyright:
© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2026
Y1 - 2026
N2 - The Artemis program intends to return humans to the Moon. With it, there has been significant international and commercial participation through mission plans for robotic landers, rovers, surface instruments, and human support systems. Many of these planned missions are intended to operate during a lunar day lasting no more than 14 Earth days. This is due to the engineering complexity of developing lunar hardware to survive the lunar night, in which temperatures can drop below-150oC for 14 days. This paper presents an integrated service hub that will store, recharge, and warm up small surface rovers, instruments, and other lunar surface vehicles at temperatures of 10-20 °C throughout the lunar night. The service hub would consist of inflatables and reinforced using RCUs or ‘smart sandbags’ and one or more towers integrated with solar panels for power generation, lighting, an integrated computing server, a data backup server, and communication antennas and receivers to permit short-range high-bandwidth communications. We consider two variations of the concept: one consisting of inflatable elements and the other of smart sandbags. The smart sandbags have integrated temperature, radiation, and IMU sensors that permit long-duration monitoring of the service hub's structural and thermal health. The “smart sandbags” would form this thermal and structural shelter at the base of this hub and house critical electronics, computers, and batteries that are otherwise sensitive to temperature.
AB - The Artemis program intends to return humans to the Moon. With it, there has been significant international and commercial participation through mission plans for robotic landers, rovers, surface instruments, and human support systems. Many of these planned missions are intended to operate during a lunar day lasting no more than 14 Earth days. This is due to the engineering complexity of developing lunar hardware to survive the lunar night, in which temperatures can drop below-150oC for 14 days. This paper presents an integrated service hub that will store, recharge, and warm up small surface rovers, instruments, and other lunar surface vehicles at temperatures of 10-20 °C throughout the lunar night. The service hub would consist of inflatables and reinforced using RCUs or ‘smart sandbags’ and one or more towers integrated with solar panels for power generation, lighting, an integrated computing server, a data backup server, and communication antennas and receivers to permit short-range high-bandwidth communications. We consider two variations of the concept: one consisting of inflatable elements and the other of smart sandbags. The smart sandbags have integrated temperature, radiation, and IMU sensors that permit long-duration monitoring of the service hub's structural and thermal health. The “smart sandbags” would form this thermal and structural shelter at the base of this hub and house critical electronics, computers, and batteries that are otherwise sensitive to temperature.
UR - https://www.scopus.com/pages/publications/105031181460
UR - https://www.scopus.com/pages/publications/105031181460#tab=citedBy
U2 - 10.2514/6.2026-2502
DO - 10.2514/6.2026-2502
M3 - Conference contribution
AN - SCOPUS:105031181460
SN - 9781624107658
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
Y2 - 12 January 2026 through 16 January 2026
ER -