Atomic number density and mass density

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SUMMARY

The discussion centers on calculating mixed number densities (MND) of UO2 fuel constituents, specifically U-238, U-235, U-234, and O-16, after exposure. Users reference the CASMO lattice code for initial calculations and discuss the method to verify these calculations by using the constant number of oxygen atoms. The solution involves dividing the number density of oxygen by 2 and adjusting for thermal expansion effects on the fuel density.

PREREQUISITES
  • Understanding of UO2 fuel composition and isotopes (U-238, U-235, U-234, O-16)
  • Familiarity with lattice codes, specifically CASMO
  • Knowledge of atomic number density and mass density calculations
  • Basic principles of thermal expansion in materials
NEXT STEPS
  • Research the CASMO lattice code for advanced fuel cycle analysis
  • Study the impact of thermal expansion on nuclear fuel properties
  • Learn about number density calculations in nuclear materials
  • Explore methods for verifying isotopic composition in nuclear fuel post-exposure
USEFUL FOR

Nuclear engineers, fuel cycle analysts, and researchers involved in nuclear fuel performance and composition verification will benefit from this discussion.

ulriksvensson
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Hello everyone. I have a problem I can't figure out.

Let's say that we start off with UO2 fuel. Knowing the density (and enrichment) we can calculate the number densities of the constituents (i.e. U-238, U-235, U-234, O-16). Suppose now that the fuel is burned to a certain exposure. A lattice code (for instance CASMO) can calculate the mixed number densities (MND). Suppose that I wanted to check this calculation backwards - given that I know the number of oxygen atoms doesn't change it should be possible. I just can't figure out how to do it.

Does anyone know how to do it? It really would help me a lot!

//Ulrik
 
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Just divide the number density of oxygen by 2! :)

(and then multiply by the atom fraction for each uranium isotope)
 
Yes I solved it the other way around:
\rho = 1/N_{a}*sum_{k=1}^{p} M_{k}*N_{k}
(Latex code)
The reason I was confues was that I forgot to compensate for thermal expansion of the fuel.
 
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