Source code for armi.materials.thoriumOxide

# Copyright 2019 TerraPower, LLC
#
# Licensed under the Apache License, Version 2.0 (the "License");
# you may not use this file except in compliance with the License.
# You may obtain a copy of the License at
#
#     http://www.apache.org/licenses/LICENSE-2.0
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# WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
# See the License for the specific language governing permissions and
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# cython: profile=False
"""
Thorium Oxide solid ceramic.

Data is from [#IAEA-TECDOCT-1450]_.

.. [#IAEA-TECDOCT-1450] Thorium fuel cycle -- Potential benefits and challenges, IAEA-TECDOC-1450 (2005).
    https://www-pub.iaea.org/mtcd/publications/pdf/te_1450_web.pdf
"""

from armi.utils.units import getTk
from armi.materials.material import Material


[docs]class ThoriumOxide(Material): name = "ThO2"
[docs] def setDefaultMassFracs(self): r"""ThO2 mass fractions. Using Pure Th-232. 100% 232 Thorium: 232.030806 g/mol Oxygen: 15.9994 g/mol 2 moles of oxygen/1 mole of Thorium grams of Th-232 = 232.030806 g/mol* 1 mol = 232.030806 g grams of Oxygen = 15.9994 g/mol* 2 mol = 31.9988 g total=264.029606 g. Mass fractions are computed from this.""" self.setMassFrac("TH232", 0.8788) self.setMassFrac("O16", 0.1212)
[docs] def density(self, Tk=None, Tc=None): """g/cc from IAEA TE 1450""" Tk = getTk(Tc, Tk) return 10.00
[docs] def linearExpansion(self, Tk=None, Tc=None): r"""m/m/K from IAEA TE 1450""" Tk = getTk(Tc, Tk) self.checkTempRange(298, 1223, Tk, "linear expansionn") return 9.67e-6
[docs] def thermalConductivity(self, Tk=None, Tc=None): r"""W/m-K from IAEA TE 1450""" Tk = getTk(Tc, Tk) return 6.20
[docs] def meltingPoint(self): r"""melting point in K from IAEA TE 1450""" return 3643.0