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Hybrid Modeling Study on Grain Evolution in the Metal Welding Process and Its Potential Lunar Application Metal is most commonly used structural material in a wide range of spacecraft, and welding is the principal method for joining metal components into functional systems. However, conducting welding experiments under extreme environments—such as microgravity or vacuum conditions in space—is prohibitively expensive and experimentally challenging. To overcome these limitations, multi-physics computational welding models provide a cost-effective and versatile alternative. In this work, the authors have developed a coupled thermal (fluid) microstructure simulation framework to model metal welding under varying gravity conditions. The framework integrates a mixed-mode heat transfer formulation (conduction, convection, and radiation) with molten pool fluid dynamics, enabling accurate prediction of temperature fields and weld-pool geometry. A grain growth model is further incorporated to capture the spatial and temporal evolution of microstructure, including grain size distribution and morphological transitions during solidification. This approach provides detailed insight into molten pool evolution and grain-level microstructure development throughout the welding process. By explicitly parameterizing environmental conditions, the model supports extrapolation to off-Earth manufacturing scenarios such as welding on the lunar surface. Tantalum—chosen in this study due to its high melting point, oxidation resistance, and mechanical stability at elevated temperatures—serves as the material system for model demonstration. Beyond Tantalum, the integrated multi-physics framework offers broad applicability for predictive welding simulations of various structural and refractory metals or alloys used in extreme terrestrial or extraterrestrial environments.
Document ID
20260002019
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Wei Li
(The University of Texas at Dallas Richardson, United States)
Fredrick N Michael
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
March 6, 2026
Publication Date
March 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Structural Mechanics
Metals and Metallic Materials
Mechanical Engineering
Report/Patent Number
NASA/TM-20260002019
Funding Number(s)
OTHER: 80NSSC25K7281
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
kinetic Monte Carlo (SPPARKS)
Grain Growth and Nucleation
Melt and Solidification
Welding
Materials and Processes
Lunar Gravity
Microgravity
Welding model
thermos-fluid model
Kinetic Monte Carlo Potts model
microstructure evolution
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