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Article

Lunar Robotic Construction System Using Raw Regolith:Design Conceptualization

1
University of Toronto Institute for Aerospace Studies (UTIAS), Toronto, ON M3H 5T6, Canada
2
MDA Space Ltd., Brampton, ON L6Y 6K7, Canada
*
Author to whom correspondence should be addressed.
Aerospace 2025, 12(11), 947; https://doi.org/10.3390/aerospace12110947
Submission received: 20 August 2025 / Revised: 8 October 2025 / Accepted: 9 October 2025 / Published: 22 October 2025
(This article belongs to the Special Issue Lunar Construction)

Abstract

This paper outlines the inception, conceptualization and primary morphological selection of a robotic system that employs raw lunar regolith for constructing protective berms and shelters on the Moon’s surface. The lunar regolith is considered the most readily available material for in situ resource utilization on the Moon. The lunar environment is characterized, and the operational task is defined, informing the development of high-level system requirements and a functional analysis through the glass-box method. The key morphological areas are identified, and candidate concepts are evaluated using the Analytic Hierarchy Process (AHP). The evaluation process employs a new approach to aggregating expert data through the ZMII method to establish priorities of the design criteria, which eliminates the need for pairwise comparisons in data collection. Each criterion is associated with a specific and quantifiable metric, which is then used to evaluate the morphologies during the AHP. The selected morphologies are determined as: a vibrating hopper for intake (normalized decision value of 27.5% out of 5 candidate solutions), a roller system for container deployment and filling (26.2% out of 7), a magnetic RCU interface (22.6% out of 7), and a 4-DoF manipulator to place the RCUs in the environment (23.6% out of 5). The final morphology is selected by combining the decision values across the primary morphological areas into a unified decision metric. This is followed by the preliminary selection of the system’s surrounding architecture. The design conceptualization is performed within a real-life operational scenario, namely, to create a blast berm for the landing pad using the lunar regolith provided by an existing excavator. The next phase of the work will include the system’s detailed design, as well as investigations on the requirements for a variety of construction tasks on the lunar surface.
Keywords: lunar construction; robotic construction; in situ resource utilization; lunar regolith; robot design conceptualization; analytic hierarchy process lunar construction; robotic construction; in situ resource utilization; lunar regolith; robot design conceptualization; analytic hierarchy process

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MDPI and ACS Style

Vasudeva, K.; Emami, M.R. Lunar Robotic Construction System Using Raw Regolith:Design Conceptualization. Aerospace 2025, 12, 947. https://doi.org/10.3390/aerospace12110947

AMA Style

Vasudeva K, Emami MR. Lunar Robotic Construction System Using Raw Regolith:Design Conceptualization. Aerospace. 2025; 12(11):947. https://doi.org/10.3390/aerospace12110947

Chicago/Turabian Style

Vasudeva, Ketan, and M. Reza Emami. 2025. "Lunar Robotic Construction System Using Raw Regolith:Design Conceptualization" Aerospace 12, no. 11: 947. https://doi.org/10.3390/aerospace12110947

APA Style

Vasudeva, K., & Emami, M. R. (2025). Lunar Robotic Construction System Using Raw Regolith:Design Conceptualization. Aerospace, 12(11), 947. https://doi.org/10.3390/aerospace12110947

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