Comprehensive nuclear materials 2 03 thermodynamic and thermophysical properties of the actinide nitrides Comprehensive nuclear materials 2 03 thermodynamic and thermophysical properties of the actinide nitrides Comprehensive nuclear materials 2 03 thermodynamic and thermophysical properties of the actinide nitrides Comprehensive nuclear materials 2 03 thermodynamic and thermophysical properties of the actinide nitrides
Trang 1the Actinide Nitrides
M Uno
University of Fukui, Fukui, Japan
T Nishi and M Takano
Japan Atomic Energy Agency, Tokai-mura, Ibaraki, Japan
ß 2012 Elsevier Ltd All rights reserved.
HD (diamond point) Hardness
LTE Linear thermal expansion
Uranium nitride UN not only has the same isotropic
a higher melting point, higher metal atom density, and
thus has advantages as a nuclear fuel compared to
proper-ties have been known for a long time However, UNhas some disadvantages as a nuclear fuel because of its
61
Trang 2Plutonium nitride and thorium nitride have been
also well studied, mainly with regard to their
suitabil-ity as nuclear fuels Other actinide nitrides with
higher atomic number are also important as potential
nuclear fuels but the data on these fuels are
insuffi-cient because they are difficult to obtain and handle
In this section, the physicochemical properties of
the actinide nitrides, mainly uranium nitrides and
plutonium nitride, are discussed First of all, phase
stability and crystal structures of the nitrides are
described Then, their thermal, thermodynamic, and
mechanical properties which are relevant to their
suitability as nuclear fuels, are discussed
Character-istics of their preparation and irradiation as nuclear
Structure
References for specific data are given separately for
each section below, but readers are also referred to a
the viewpoint of suitability as nuclear fuels, the
vari-ous properties of not only the nitrides but also the
other compounds The binary phase diagram shown
inFigure 12is taken from data published in 1960,3–7
and is still valid The phase stability of U–N systems
an NaCl-type cubic structure, and the latter has an
nitrogen pressure (126 atm); and its lattice parameterdecreases with an increase in nitrogen content The
Although the phase diagram, where nitrogen
have a wide range of nonstoichiometry, at lowernitrogen pressure; UN decomposes such that UN
Figure 312,13; here theb-U2N3in the previous graph
nitrogen pressure of 2 atm is reported to be nearly
decomposes to U and nitrogen at nitrogen pressurebelow 2.5 atm As the decomposition of UN mustinfluence the properties of the fuel pellets, and the
forma-tion of UN through carbothermic reducforma-tion, the
important from the viewpoint of their use as nuclear
12 10 8 6
4 2
PN2>> 10 5 Pa
Figure 1 U–N phase diagram at nitrogen pressure larger
than 105 Pa Data from Levinskii, Yu V Atom Energ 1974,
37(1), 216–219; Sov Atom Energ (Engl Transl.) 1974,
37(1), 929–932.
(c)
U N
Figure 2 Crystal structures of (a) UN, (b) a-U 2 N 3 , and (c) b-U N
Trang 3fuel The reported decomposition curves are shown in
Figure 4.3It is seen from these graphs, for example,
1620 K at nitrogen pressure of 1 atm More detailed
decomposition behavior of UN as well as other
only one structure for the mononitride, PuN: an
NaCl-type face-centered cubic (fcc) structure with
a ¼ 4.904 A˚ PuN is a line compound with little
non-stoichiometry, and is reported not to congruently
there is a study on the safety assessment of fuels on
the basis of vaporization behavior in which the
melt-ing temperature of Pu–N is given as 2993 K under a
Though thorium is a fertile material, recent research
on thorium and its compounds as nuclear fuel is
the former is an NaCl-type cubic structure with
UN 2
10 5 Pa
UN2+
N 2
a-U + UN b-U + UN
Figure 3 U–N phase diagram at nitrogen pressure smaller
than 2 atm Data from Storms, E K Special Report to the
Phase Equilibria Program; American Ceramic Society:
Westerville, OH, 1989; Muromura, T.; Tagawa, H J Nucl.
1 2
5 6
P Gross, C Hayman and H Clayton, ‘‘Heats of Formation
of Uranium Silicides and Nitrides’’; In Thermodynamics of Nuclear Materials- Proceedings of Symposium on Thermodynamics of Nuclear Materials, Vienna, May 1962, International Atomic Energy Agency.
Trang 42 atm Hypo- and hyper-ThN appear above 1350C.
important to consider the temperature and nitrogenand oxygen pressures during the preparation of ThN
Curium NitridesThese nitrides are also usually prepared by car-
difficult to prepare bulk samples due to their highradioactivity, there have been no systematic studies
on their phase stability However, it has been lished that there is only mono nitride in these systemsfrom the fact that no nitrogen absorption occurredupon cooling in nitrogen atmospheres during car-bothermic reduction These mono nitrides have anNaCl-type face-centered cubic structure, and their
structure of these three nitrides, as well as uraniumand plutonium nitrides, is advantageous as nuclear
g b 500
-483 ⬚C -483 ⬚C -320⬚C -215 ⬚C -125⬚C
N solubility in Th (Gerds and Mallett) 115
ThN + fccTh
ThN + bccTh
Th3N4+ ThN
1800 ⬚ ± 25 ⬚
1605 ⬚ ± 20 ⬚
Figure 6 Phase diagram of Th–N system Reproduced
from Benz, R.; Hoffman, C G.; Rupert, G N J Am Chem.
Soc 1967, 89, 191–197, with permission from Elsevier.
Trang 5fuels, especially as accelerator-driven system (ADS)
targets of nitride solid solutions that contain a large
amount of minor actinides (MAs) Experimental
research on their vaporization behavior has revealed
that the congruent melting temperature of NpN was
stability and other properties of pure CmN Some data
on Cm and U or Pu solid solutions have been reported,
and these will be discussed in the next section
Mixtures
As (U,Pu)N were some of the most promising
candidates for the first breeder reactors, they are the
best studied nitride solid solution fuels UN and PuN
form a continuous solid solution, and the lattice
param-eter increases with an increase in the plutonium
con-tent, and is accompanied by a large deviation from
nonideality of the solution A diagram of the calculated
suggests that there is a relatively narrow range of
pos-sible (U,Pu)N compositions, as is the case with U–N
and Pu–N binary systems It is suggested that the
As uranium monocarbide and plutonium
mono-carbide, as well as other actinide carbides, have an
NaCl-type fcc structure, actinide nitrides and
acti-nide carbides form solid solutions Some research
performed on actinide nitride carbides, for example,
suit-ability of these carbonitride fuels and the impurities
in nitride fuels after carbothermic reduction Phase
stability graphs of U and/or Pu–N–C, both with andwithout oxygen, also have been constructed in order
behav-ior of (U and/or Pu)–N–C fuels also has been
scope of this chapter
As MAs are usually burnt with uranium and tonium for transmutation, and as Am originally exists
plu-in Pu, (MA,U)N or (MA,Pu)N have also been wellstudied As mentioned above, the vaporization behav-
vaporization of Pu and Am was observed The latticeparameters of (U,Np)N and (Np,Pu)N increase withincrease in Np and Pu content, and with a small
Although scarcely any data for pure CmN has been
Inert matrix fuels, where MA as well as uraniumand plutonium are embedded in a matrix, are alsobeing considered for use in ADS for transmutation.Recent research in MAs has focused on using variousnitride solid solutions and nitride mixtures as inertmatrix fuels For ADS targets, matrices have beendesigned and selected so as to avoid the formation
of hot spots and to increase the thermal stability,especially in the case of Americium nitride Con-sidering their chemical stability and thermal conduc-tivity, ZrN, YN, TiN, and AlN were chosen as
Table 1 Lattice parameter of some actinide nitrides
Source: Minato, K.; et al J Nucl Mater 2003, 320, 18–24, with
permission from Elsevier.
UN−NpN
Vegard’s law
0.8 1 0.6
Composition
0.4 0.2 0
0.4890
0.4895 0.4900 0.4905
UN UN NpN
PuN NpN PuN
UN−PuN NpN−PuN
Figure 7 Lattice parameter of some actinide nitride solid solution Reproduced from Minato, K.; et al J Nucl Mater 2003, 320, 18–24.
Trang 6fcc structure with a ¼ 4.580 A˚ and has nearly the same
thermal conductivity as UN, has a high melting point,
good chemical stability in air, and a tolerable
dissolu-tion rate in nitric acid Recently, abundant data
have been made available for ZrN-based inert matrix
fuels It is planned that (Pu,Zr)N, with about 20–25%
The lattice parameter of (Pu,Zr)N decreases with an
increase in the Zr content, and is between that of
It has also been estimated, using a model, that (Pu,Zr)N with 20–40 mol% PuN, does not melt till up
to 2773 K; this is based on experimental
reported that two solid solutions are obtained when
Am content of the two phases have been estimated,from the lattice parameter, to be 14.5 and 43.1 mol%
A thermodynamic modeling of a uranium-free inert
PuO2
PuN
CmN CmO2
CmO2
0.6 0.8 1
PuO2
CmN
Figure 9 Lattice parameter of (Pu,Cm)N and (Pu,Cm)O 2
Reproduced from Minato, K.; et al J Nucl Mater 2003,
320, 18–24, with permission from Elsevier.
Trang 7matrix fuel, for example, (Am0.20Np0.04Pu0.26Zr0.60),
In contrast to ZrN, TiN does not dissolve MA
nitrides even though TiN also has an NaCl-type fcc
structure This is explained by the differences in
A mixture of PuN and TiN was obtained by several
heat treatments above 1673 K, and the product, in
which one phase was formed, did not contain the
may be hypostoichiometric although (Pu,Zr)N is
hyperstoichiometric
In this section, the melting points and decomposition
temperatures of actinide mononitrides are discussed
in conjunction with the nitrogen pressures because
this behavior depends on the nitrogen partial
pres-sure of the system The vapor prespres-sure of a metal gas
over the solid nitride is discussed in the next section
as ‘vaporization behavior.’
The liquid mononitride MN (liq.) can be observed
when congruent melting occurs under a pressurized
nitrogen atmosphere; otherwise the solid
mononi-tride MN (s) decomposes into nitrogen gas and liquid
metal that is saturated with nitrogen, according to the
following reaction,
Olson and Mulford have determined the
by the optical observation of the nitride granules
when they were heated under controlled nitrogen
the nitrogen pressure p (atm) in logarithmic scale and
The solid curves show the following equations:
atm) The congruent melting for PuN was notachieved in the nitrogen pressure range up to 24.5 atm.The presence of an oxide phase, as an impurity,seems to lower the melting point and decompositiontemperature In the case of ThN mentioned above,the melting point and decomposition temperature
of a specimen containing 0.6 wt% oxygen fell by
130 K from those of the oxygen-free specimens( 0.04 wt% oxygen) A similar experiment conducted
that has the same crystal structure, has revealed adecrease in the melting point by 200–300 K when theoxygen content increased from 0.15 to 0.5–1.0 wt%.Some data sets on the equilibrium nitrogen pres-
Congruent melting
ThN
3.2 3
Trang 8U(C,N), as measured by the Knudsen-cell and
mass-spectroscopic technique at lower temperatures, are
curve represents the correlation for UN developed
given as:
with a decrease in x, together with a lowering in the
is approximately one-fifth of that of UN When
con-sidering a nitride or carbide as nuclear fuel for fast
reactors, it should be noted that the decomposition
pressure of nitrogen can be lowered and that the
reactivity of carbide with moisture can be moderated
by employing the carbonitride instead of the nitride
or carbide
No experimental data on the melting behavior of
transplutonium nitrides such as AmN and CmN have
relationship between the decomposition temperatureand the instantaneous coefficients of linear thermalexpansion (CTE) and used it to predict the decom-
CTE at 293 and 1273 K plotted against reciprocaldecomposition temperature under 1 atm of nitrogenfor some transition metal nitrides (TiN, ZrN, HfN)and actinide nitrides (UN, NpN, PuN) The data used
references Except for the large CTE value for PuN at
293 K, a reasonable linear relationship is shown by theagreement of the broken lines From the CTE valuesfor AmN, determined by the high-temperature X-raydiffraction technique, the decomposition temperature
of AmN under 1 atm of nitrogen was roughly dicted to be 2700 K, which is much lower than that
pre-of PuN
In this section, the vapor pressure of a metal gas over
a solid actinide nitride is summarized
Timofeeva Brundiers TPRC Smirnov Houska
Kruger Benedict Aldred Takano
2.6 4 6 8 10 12 14
Figure 13 Coefficients of linear thermal expansion at 293 (open symbols) and 1273 K (closed symbols) for some transition metal nitrides and actinide nitrides plotted against reciprocal decomposition temperature under 1 atm of nitrogen For references see Table 2
8
3 4
1
2 9
5: x = 1 6: x = 0.79 7: x = 0.5 8: x = 0.36 9: x = 0.2
Figure 12 Decomposition pressures of U(C,N) as a
function of reciprocal temperature below 2400 K Solid
lines by Ikeda et al.44and broken lines by Prins et al.45
Dotted line for UN reviewed by Hayes et al.46
Trang 9The major vapor species observed over UN are
U(g) UN(g) can also be detected in addition to U(g)
mag-nitude lower than that of U(g); therefore, the
contri-bution of UN(g) can be ignored in practice Some
fitting the data from eight experimental investigations
According to that paper, the reported data on
UN(s) vary somewhat The U(g) pressure obtained by
from the equation developed by Hayes et al., but is
It is well known that the evaporation of UN is
accompanied by the precipitation of a liquid phase,
The reported vapor pressure of U(g) over UN(s) is
suggested that the dissolution of nitrogen and/or
impurity metal from crucibles into the liquid phase
could affect the observed partial pressure Some
scat-tering of the previously reported data on U(g) over
UN(s) may be also caused by a reaction of the liquid
phase in UN with the crucible material From this
viewpoint, it appears that the partial pressure of U(g)
over UN(s) should be a little higher than that posed by Hayes et al
pro-The vapor species over PuN are nitrogen
PuN(g) is not detected because PuN is more unstable
Table 2 Summary of melting point, decomposition temperature and linear thermal expansion coefficient (CTE) for some transition metal nitrides and actinide nitrides
Nitride Congruent
melting point (m.p.) (K)
Decomposition temperature a (K)
References CTE (106K1) References Method or
: U(g), Hayes et al.46
: U(g), Suzuki et al.61
: U(g), Alexander et al.62
Figure 14 Partial pressure of N 2 (g) and U(g) over UN (s) as a function of temperature Adapted from Hayes, S L.; Thomas, J K.; Peddicord, K L J Nucl Mater 1990, 171, 300–318; Suzuki, Y.; Maeda, A.; Arai, Y.; Ohmichi, T J Nucl Mater 1992, 188, 239–243;
Alexander, C A.; Ogden, J S.; Pardue, W H J Nucl Mater 1969, 31, 13–24.
Trang 10Pardue et al.,66and Campbell and Leary.67These dataseem to agree with each other.
The vapor pressure of Pu(g) over PuN(s), as a
values reported in the different studies almost
range of 1400–2400 K, which suggests that PuN
Pu(g) over PuN(s), at temperatures lower than
1600 K, is a little higher than the values extrapolatedfrom the high-temperature data, and that it approachesthat over Pu metal with further decrease in tempera-ture There is some possibility that a liquid phaseforms at the surface of the sample during the coolingstages of the mass-spectrometric measurements,because PuN has a nonstoichiometric compositionrange at elevated temperatures, while it is a linecompound at low temperatures
The vapor pressure of U(g) and Pu(g) over UN(s),
Table 3gives the vapor pressures of U(g) and Pu(g)
logarithmic temperature coefficients It is noteworthythat the vapor pressure of Pu(g) over mixed nitridewas observed to increase with an increase in the PuNcontent
of Np(g) over NpN(s) in the temperature range of1690–2030 K by using the Knudsen-cell effusion mass
function of temperature The partial pressure of Np(g) can be expressed using the following equation:
The vapor pressures of Np(g) over NpN(s) obtained
by Nakajima et al are similar to those of Np(g) over
10 4/T (K–1 ) 4.5 5.0 5.5 6.0 6.5 7.0 7.5
Figure 15 Partial pressure of Pu(g) over PuN(s) as a
function of temperature Data from Suzuki, Y.; Maeda, A.;
Arai, Y.; Ohmichi, T J Nucl Mater 1992, 188, 239–243;
Kent, R A.; Leary, J A High Temp Sci 1966, 1, 176–183;
Sheth, A.; Leibowitz, L ANL-AFP-2, Argonne National
Laboratory; Chemical Engineering Division: Argonne,
: (U0.80Pu0.20)N : (U0.65Pu0.35)N : (U0.40Pu0.60)N : (U0.20Pu0.80)N : PuN
Figure 16 Partial pressure of U(g) and Pu(g) over UN(s),
PuN(s) and mixed nitride as function of temperature.
Reproduced from Suzuki, Y.; Maeda, A.; Arai, Y.; Ohmichi,
T J Nucl Mater 1992, 188, 239–243.
Table 3 Partial pressure of U and Pu over UN, PuN, and (U,Pu)N
Compound Vapor species Vapor pressure log p (Pa) Temperature range (K)
Trang 11liquid Np metal found by Ackermann and Rauh71;
decomposition mechanism is considered to be
of Am(g) over AmN by using values of the Gibbs
The evaporation of AmN obeys the following
vapor pressure of Am over AmN, expressed as a
function of temperature, is
log p AmðgÞðPaÞ ¼ 12:913 20197=T
The calculated vapor pressures of Am over AmN are
The vapor pressure of Am over AmN is higher than
those of other actinide vapor species over their
respective nitrides
Data on the heat capacities of actinide nitrides are
very limited due to the experimental difficulties
In this section, the heat capacities of uranium nitride
UN, plutonium nitride PuN, neptunium nitride NpN,and americium nitride AmN are summarized
heat capacity of UN based on a comparison of ninedata sets; these seem to agree with each other at lowtemperatures but their data are limited, and to someextent scattered, at elevated temperatures The pre-viously reported values for the heat capacity of UNexhibit an almost linear increase with temperature,
trend at temperatures over 1500 K This behavior isanalogous to that of the actinide carbides, as pointed
the results of Conway and Flagella Thus, the heatcapacity data reported by Hayes et al can be consid-ered reliable The heat capacity of UN, expressed byHayes et al., is as follows:
Information on the heat capacity of PuN is veryscarce and is limited to the low temperatures More-over, the two data sets on PuN given by Alexander
Pu(g) over PuN Np(g) over NpN
Figure 17 Temperature dependence of partial pressure of
Np(g) over Np(1), Np(g) over NpN(s) and Am(g) over AmN(s)
together with those of U(g) and Pu(g) over UN(s) and PuN(s)
as a function of temperature Adapted from Suzuki, Y.;
Maeda, A.; Arai, Y.; Ohmichi, T J Nucl Mater 1992, 188,
239–243; Nakajima, K.; Arai, Y.; Suzuki, Y J Nucl Mater.
1997, 247, 33–36; Ackermann, R J.; Rauh, E G J Chem.
Thermodyn 1975, 7, 211–218; Takano, M.; Itoh, A.;
Akabori, M.; Minato, K.; Numata, M In Proceedings of
GLOBAL 2003, Study on the Stability of AmN and (Am,Zr)N,
New Orleans, LA, Nov 16–20, 2003; p 2285, CD-ROM.
500 50
60 70
1000 1500 2000
Figure 18 Heat capacities of PuN Data from Alexander,
C A.; Clark, R B.; Kruger, O L.; Robins, J L Plutonium and Other Actinides 1975; North-Holland: Amsterdam, 1976; pp 277; Oetting, F L J Chem Thermodyn 1978, 10, 941–948.
Trang 12et al.65 and Oetting75are not consistent Matsui and
of PuN and have argued that the Oetting correlation
is more reliable Therefore, the heat capacity data, as
reported by Oetting, is given here The heat capacity
function of PuN given by Oetting is
The heat capacities of UN, PuN, and (U,Pu)N are
solutions can be estimated from those of its raw
materials with the same structure on the basis of the
additive law, it can be expected that the values for
the (U,Pu)N solid solutions are an intermediate
between those of UN and PuN However, the heat
capacities of (U,Pu)N, as reported by Alexander
UN, by Hayes et al., and PuN, by Oetting In addition,
the temperature dependencies of the heat capacities
of PuN and its solid solutions are almost linear,
although it has been suggested that they can shift
toward larger values at elevated temperatures, as
does UN It is considered that these discrepancies
are probably due to the lack of experimental data
Thus, it is necessary to obtain the accurate heat
capacity of PuN and (U,Pu)N
Recently, the heat capacities of NpN and AmN
of NpN and AmN were prepared by the carbothermicreduction of their respective oxides The enthalpyincrements were measured using a twin-type dropcalorimeter in a glove box The heat capacities weredetermined by derivatives of the enthalpy increments.The measured heat capacity of NpN is expressed by
distinct differences, the heat capacity of AmN wasslightly lower than those of UN, NpN, and PuN.The heat capacities of (Np,Am)N and (Pu,Am)Nsolid solutions were also obtained The heat capa-cities decreased slightly with an increase in Amcontent This tendency was attributed to the heatcapacity of AmN being slightly smaller than those
Some data on the Gibbs free energy of formation foractinide nitrides exist In this section, the Gibbs freeenergy of formation of uranium nitride, UN, pluto-nium nitride, PuN, uranium and plutonium mixednitride, (U,Pu)N, neptunium nitride, NpN, andamericium nitride, AmN are summarized
Figure 19 Heat capacities of UN, PuN, and (U,Pu)N Data
from Hayes, S L.; Thomas, J K.; Peddicord, K L J Nucl.
Mater 1990, 171, 300–318; Oetting, F L J Chem.
Thermodyn 1978, 10, 941–948; Alexander, C A.;
Ogden, J S.; Pardue, W M Thermophysical properties of
(UPu)N In Plutonium 1970 and Other Actinides PT.1; 1970,
17, 95–103; Kandan, R.; Babu, R.; Nagarajan, K.; Vasudeva
Rao, P R Thermochim Acta 2007, 460, 41–43.
400 0 20 40 60 80