NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Enabling Nuclear and Solar Thermal Propulsion with the Computational Laboratory: Faster and Cheaper Materials CharacterizationNuclear and solar thermal propulsion offer enhanced efficiencies for in-space travel which may open up the outer Solar System to both crewed and automated craft. However, these advanced propulsion systems require cutting-edge materials which are often not easily tested in the laboratory. Ab initio thermodynamics and other computational methods offer a way to test materials at high pressures and temperatures more quickly, and with reduced cost. Here, several case studies are presented which highlight the utility of modern simulation techniques. First, an extensive thermodynamic study was performed at the ab initio level to elucidate the role of hot hydrogen flow on the erosion of four refractory carbides to examine their appropriateness for use as channel coatings. A detailed analysis of reaction products informs estimates of erosion which are validated in comparison with heritage NERVA data. Specific material suggestions are made for both nuclear and solar designs. Secondly, we examined the mechanical behavior and chemical stability of various components of an idealized nuclear cermet core design using techniques spanning from the atomic to microscale. Next, the mechanical and chemical behavior of tungsten (a potential matrix material) and the stability of uranium mononitride (a potential ceramic fuel element), are characterized in the presence of hydrogen and at elevated temperatures with ab initio thermodynamics. Finally, the mechanical response and failure of tungsten under tensile strain is simulated at the micron scale with a combined finite element and dislocation dynamics approach. The resultant stress-strain data agrees well with experiments and leads to a workflow which can incorporate ab initio thermodynamic data into micron-scale simulations and thus provide real-world relevant estimates of erosion and stress-strain behavior. The power of this framework and our plans to use it in the future will be discussed.
Document ID
20210015849
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
William C Tucker
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Piyas Chowdhury
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Lauren J Abbott
(Ames Research Center Mountain View, California, United States)
Charles W Bauschlicher
(Ames Research Center Mountain View, California, United States)
Dean Cheikh
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Michael Preudhomme
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Justin B Haskins
(Ames Research Center Mountain View, California, United States)
Date Acquired
May 19, 2021
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 2021 National Space & Missile Materials Symposium (NSMMS) and the 2021 Commercial and Government Responsive Access to Space Technology Exchange (CRASTE)
Location: Online
Country: US
Start Date: June 21, 2021
End Date: June 25, 2021
Sponsors: Blue52 Productions LLC
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available