Abstract
Carbides of uranium have attracted interest as fuels for nuclear thermal propulsion (NTP) to drive deep-space exploration owing to their attractive thermal and neutronic properties. Optimization of NTP technology, however, requires ultra-high temperature reactor environments to maximize the ratio of thrust to propellant to achieve peak rocket engine efficiency. Incorporation of transition metals into uranium carbides offers a pathway to increase the melting point of carbide fuels to address the operational challenges posed by NTP. A thermodynamic model has been developed to examine the phase relationships in the C–Ti–U system at NTP conditions. Calculated phase relationships at ultra-high temperatures predict a stable (U, Ti)C solid solution. Additionally, experimental work on C–Ti–U synthesis via arc melting has been carried out, providing data on phase constitution and compositions that can be used to further refine the thermodynamic model that has been developed.
Original language | English |
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Pages (from-to) | 3519-3527 |
Number of pages | 9 |
Journal | JOM |
Volume | 73 |
Issue number | 11 |
DOIs | |
State | Published - Nov 2021 |
Funding
The authors gratefully acknowledge the support of the U.S. Department of Energy through the LANL/LDRD Program and the G. T. Seaborg Institute for this work. The authors would also like to thank John Dunwoody for assistance with arc melting and Scarlett Widgeon Paisner for insightful discussion.
Funders | Funder number |
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G. T. Seaborg Institute | |
U.S. Department of Energy | |
Laboratory Directed Research and Development | |
Los Alamos National Laboratory |