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Homogeneity Study of ZrC, NbC, and TaC Binary Carbide Fuels for the Application of Nuclear Thermal PropulsionIn alignment with NASA and DARPA goals, efforts towards Nuclear Thermal Propulsion (NTP) have increased in recent years. As progress is made, a main challenge still exists; the fuel in an NTP system must survive the extreme environment experienced during operating conditions. Three fuel forms have been studied including a ceramic-metallic matrix, a ceramic-ceramic matrix, and solid solution carbides. Solid solution carbides were studied previously as a fuel for NTP and was shown to be a promising technology; however, the programs were canceled before demonstration in an NTP engine test. Of the refractory metal carbides of interest, zirconium carbide (ZrC), niobium carbide (NbC) and tantalum carbide (TaC) were studied. ZrC, NbC, and TaC powders were consolidated in monocarbide (ZrC, NbC, TaC) and bi-carbide (ZrC-NbC, ZrC-TaC, NbC-TaC) forms using spark plasma sintering (SPS), with 50-50 mol% compositions of the bi-carbides of interest. The time and temperature conditions to achieve a completely homogeneous solid solution for the mixed carbides is of interest for NTP fuel applications, since this homogeneity is considered to be essential for this fuel form. Homogeneity is typically not achieved during sintering, as surface diffusion (predominant for sintering to near ideal density) tends to occur at lower temperatures than bulk volumetric diffusion (required for solute interdiffusion to achieve a homogeneous solid solution). High temperature isochronal annealing was performed to identify the conditions to achieve a chemically homogeneous sample. The solute interpenetration vs annealing temperature was quantified using energy dispersion spectroscopy (EDS) in a scanning electron microscope (SEM). X-ray diffraction (XRD) was used to accurately measure the phase stability and lattice parameter as a function of annealing conditions. The diffusion data from each sample was then used to determine self-diffusion coefficients for interdiffusion of the Nb, Zr, and Ta solutes and compared to existing literature values. The minimum annealing conditions to achieve complete chemical homogeneity for each carbide was determined.
Document ID
20230006519
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Alexander T Nadermann
(University of Tennessee at Knoxville Knoxville, Tennessee, United States)
Jonas R Kessing
(University of Tennessee at Knoxville Knoxville, Tennessee, United States)
Brandon Shaver
(University of Tennessee at Knoxville Knoxville, Tennessee, United States)
Justin Milner
(Glenn Research Center Cleveland, Ohio, United States)
Kelsa Palomares
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Steven J Zinkle
(University of Tennessee at Knoxville Knoxville, Tennessee, United States)
Date Acquired
April 27, 2023
Publication Date
May 8, 2023
Publication Information
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space Conference
Location: Idaho Falls, ID
Country: US
Start Date: May 8, 2023
End Date: May 11, 2023
Sponsors: American Nuclear Society
Funding Number(s)
CONTRACT_GRANT: 80NSSC20K1434
CONTRACT_GRANT: 80LARC17C0003
CONTRACT_GRANT: 80NSSC21K2011
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
nuclear thermal propulsion
solid solution carbides
spark plasma sintering
zirconium carbide
niobium carbide
tantalum carbide
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