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Structural Sizing of a 50-m-Tall Thermoplastic Composite Truss Tower Structure for the Lunar South PoleAt the lunar south pole, solar arrays elevated by truss towers are exposed to near continuous sunlight since the sun remains near the horizon. Recent studies suggest that tower heights on the order of 50 m are needed to meet the power requirements to support a sustained lunar presence. While eventually towers may be constructed using materials sourced in-situ, initially structural elements will likely be brought from the Earth, deployed, and assembled. Thermoplastic composites offer the benefit of high specific stiffness and strength properties along with welding for assembly joints, and therefore represent a promising material system for this application. The focus of this paper is on the structural sizing of such towers. A set of expressions based on beam theory are presented for preliminary sizing of the truss tower structure for strength and buckling. The loading condition that drives sizing is base excitation resulting from moonquakes. A point design, developed through finite element analysis, verifies the analytical sizing routine and shows the importance of joints. The results show a viable point design and highlight the factors most significant in the structural sizing.
Document ID
20250001459
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Andrew C Bergan ORCID
(Langley Research Center Hampton, United States)
Arunkumar Satyanarayana
(Langley Research Center Hampton, United States)
Will J Grier
(Langley Research Center Hampton, United States)
Babak Farrokh
(Goddard Space Flight Center Greenbelt, United States)
Kenneth N Segal
(Heliospace Corporation Greenbelt, Maryland)
John Chiu
(Actalent Corporation Greenbelt, Maryland)
Sandi Miller
(Glenn Research Center Cleveland, United States)
Date Acquired
February 6, 2025
Publication Date
February 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Structural Mechanics
Composite Materials
Report/Patent Number
NASA/TM-20250001459
Funding Number(s)
WBS: 264925.04.27.23
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Thermoplastic composites
Lunar structures
Structural sizing
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