Calculating Atom Density of UO2-ThO2 Fuel

  • Thread starter Thread starter tony.almeda
  • Start date Start date
  • Tags Tags
    Atom Density Fuel
AI Thread Summary
To calculate the number density of a fuel composition with 75 wt% ThO2 and 25 wt% UO2, where U enrichment is 19.5 w%, use the formula N = (Rho * NA) / A, where Rho is the density in g/cm^3, NA is Avogadro's number, and A is the atomic weight in g. The composite number density can be determined by weighing the contributions of each nuclide based on their proportions in the mixture. This includes calculating the number densities for Thorium and the two isotopes of Uranium, U-235 and U-238. Additionally, the discussion suggests that the inquiry may relate to finding the macroscopic cross-section, which involves multiplying the number density by the microscopic cross-section measured in barns. Understanding these calculations is essential for accurate nuclear fuel analysis.
tony.almeda
Messages
3
Reaction score
0
if fuel coposition as follow : 75 wt% Tho2- 25 wt% uo2, were the U enrichment 19.5 w% ... how can i caculate the number density (Atoms/barn-cm) for the comopsition ?
 
Engineering news on Phys.org
If I recall correctly number density of a nuclide is just the number of atoms per unit volume as given by;

N = (Rho * NA) / A

Where; Rho = density (in g/cm^3)
NA = Avagadro number
A = Atomic weight in g

To find the composite for the mixture just weight by the relative proportions of the nuclides in the mixture.

i.e [0.75*N(Thorium)] + [0.25*0.195*N(U-235)] + [0.25*(1-0.195)*N(U-238)]

From your query I wonder if you are really after the macroscopic cross-section which is simply the number density multiplied by the microscopic cross-section (as measured in barns).
 
Last edited:
Hello everyone, I am currently working on a burnup calculation for a fuel assembly with repeated geometric structures using MCNP6. I have defined two materials (Material 1 and Material 2) which are actually the same material but located in different positions. However, after running the calculation with the BURN card, I am encountering an issue where all burnup information(power fraction(Initial input is 1,but output file is 0), burnup, mass, etc.) for Material 2 is zero, while Material 1...

Similar threads

Back
Top