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Advanced Materials for the Lunar Surface: Multiscale Computational Design of Refractory Alloys and CarbidesEmerging operational environments, such as the lunar surface, present novel challenges for NASA and drive the need for advanced materials in applications like fission surface power systems. To address these demands, computational materials science is rapidly evolving to augment or replace costly and hazardous empirical testing. Although materials selection at NASA remains predominantly experimentally driven, advanced simulation methodologies are being steadily integrated into the engineering lifecycle. This work details the application of multiscale simulation techniques—including first-principles calculations, CALPHAD, dislocation dynamics, and molecular dynamics—at NASA's Ames Research Center to evaluate advanced materials for extreme environments.

First, we present contributions to the Space Nuclear Propulsion Project. Be-cause propellant channel coatings in nuclear thermal rockets must withstand high-pressure, high-temperature hydro-gen, optimizing these materials is critical. First-principles calculations were employed to establish a rigorous quantitative and qualitative understanding of the behavior of the refractory carbides ZrC, NbC, and their mixtures in high-enthalpy hydrogen environments. This necessitated the generation of high-fidelity thermodynamic models for both stoichiometric and carbon-depleted carbides, both with and without the presence of hydrogen.

Furthermore, we highlight efforts under the Refractory Alloy Additive Manufacturing Build Optimization (RAAMBO) project, where existing and novel alloy compositions were assessed for additive manufacturing printability and subsequent performance in applications such as heat pipes and rocket nozzle extensions. This was accomplished through a comprehensive multiscale simulation framework that bridged the gap from the nanometer to the millimeter scale.

Across both initiatives, rigorous validation against empirical data was prioritized. By systematically employing a verified and validated computational frame-work, we demonstrate how simulation effectively supports multidisciplinary engineering efforts, builds project-wide confidence, and drives critical materials development.
Document ID
20260003271
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
William C Tucker
(Analytical Mechanics Associates (United States) Hampton, United States)
Jaehyun Cho
(Analytical Mechanics Associates (United States) Hampton, United States)
Justin B Haskins
(Ames Research Center Mountain View, United States)
Lauren J Abbott
(Ames Research Center Mountain View, United States)
Date Acquired
April 20, 2026
Subject Category
Lunar and Planetary Science and Exploration
Meeting Information
Meeting: 2026 Lunar Surface Innovation Consortium Spring Meeting
Location: Washington, DC
Country: US
Start Date: April 28, 2026
End Date: April 30, 2026
Sponsors: Johns Hopkins Applied Physics Laboratory
Funding Number(s)
CONTRACT_GRANT: 80ARC025D0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
computational materials
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