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E zarkadoula zirconia
1. See discussions, stats, and author profiles for this publication at: https://www.researchgate.net/publication/260203819
High-energy radiation damage in zirconia: Modeling results
Article in Journal of Applied Physics · February 2014
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2. High-energy radiation damage in zirconia: modeling results
E. Zarkadoula,1, 2, 3
R. Devanathan,4
W. J. Weber,3, 5
M. Seaton,6
I. T. Todorov,6
K. Nordlund,7
M. T. Dove,1
and K. Trachenko1, 2
1
School of Physics and Astronomy, Queen Mary University of London, Mile End Road, London, E1 4NS, UK
2
SEPnet, Queen Mary University of London, Mile End Road, London E1 4NS, UK
3
Materials Science & Technology Division, Oak Ridge National Laboratory, Oak Ridge, TN 37831, USA
4
3 Nuclear Sciences Division, Pacific Northwest National Laboratory, Richland, WA 99352, USA
5
Department of Materials Science & Engineering,
University of Tennessee, Knoxville, TN 37996, USA
6
Scientific Computing Department, STFC Daresbury Laboratory,
Keckwick Lane, Daresbury, Warrington, Cheshire, WA4 4AD, UK
7
University of Helsinki, P.O. Box 43, FIN-00014 Helsinki, Finland
Zirconia is viewed as a material of exceptional resistance to amorphization by radiation damage,
and consequently proposed as a candidate to immobilize nuclear waste and serve as an inert nuclear
fuel matrix. Here, we perform molecular dynamics simulations of radiation damage in zirconia
in the range of 0.1-0.5 MeV energies with account of electronic energy losses. We find that the
lack of amorphizability co-exists with a large number of point defects and their clusters. These,
importantly, are largely isolated from each other and therefore represent a dilute damage that does
not result in the loss of long-range structural coherence and amorphization. We document the nature
of these defects in detail, including their sizes, distribution and morphology, and discuss practical
implications of using zirconia in intense radiation environments.
Radiation effects have been finding increasing applica-
tions in various fields with notable examples of semicon-
ductor and nuclear industries. In nuclear power applica-
tions, materials will be exposed to high dose irradiation
coming from highly energetic products of fission and fu-
sion. In these applications, the energy of emitted parti-
cles has a two-fold effect: on one the hand, this energy is
converted into useful energy, by heating the material; on
the other hand, this energy damages the material and de-
grades the properties important for the operation, includ-
ing mechanical, thermal, transport and other properties.
This is currently a central issue in the area of both fusion
and fission energy generation [1, 2]. The latter in partic-
ular faces the problem of finding a material suitable for
safe long-term encapsulation of nuclear waste [2–4]. Can-
didate materials for safe encapsulation of nuclear waste,
waste forms, need to be structurally stable and have low
diffusion rates of radioactive ions to prevent polluting the
environment. Waste forms often become amorphized by
radiation damage from the nuclear waste, with most of
amorphization produced by energetic heavy ions in colli-
sion cascades that consist of atoms displaced from their
sites [2–5]. The diffusion can dramatically increase as
a result of irradiation-induced amorphization [4, 6]. For
this reason, the search for radiation-resistant waste forms
has been on for several decades.
Zirconia, ZrO2 (both in cubic and monoclinic form),
stands out on the list of materials that are highly resis-
tant to amorphization: both in-situ and ex-situ experi-
ments such as X-ray diffraction, Rutherford backscater-
ring spectroscopy, transmission electron microscopy and
so on indicated no loss of crystalline structure in bulk
samples under bombardment with heavy MeV-energy
ions and plutonium doping [7–14]. This was considered as
evidence for the exceptional resistance to amorphization
compared to other materials [15, 16] and, combined with
its ability to incorporate radioactive ions from nuclear
waste including actinides [17], zirconia has been consid-
ered as a strong candidate material for inert fuel and
nuclear waste matrices [2, 7–14, 18–22].
An important question arises regarding what the high
resistance to amorphization implies for the purposes of
using zirconia as a waste form. The experimental probes
above provide the information about the long-range or-
der, and in many cases do not directly probe the nature of
point defects and clusters smaller than several nanome-
ters. Instead, these probes study the macroscopic con-
sequences such as lattice swelling. This issue has been
recently receiving increasing attention in the context of
elucidating the local, as opposed to long-range, structure
[23]. In the case of zirconia, point defects and small clus-
ters of point defects may not affect the Bragg peaks up
to the smallest k-numbers, yet play an important role in
defect-assisted diffusion processes involving the radioac-
tive ions. Point defects have been seen in irradiated zir-
conia, although determination of their exact structure,
abundance and distribution have been viewed as chal-
lenging [7–14]. In this paper, we address this question
using molecular dynamics (MD) simulations, a method
that provides access to detailed structural changes at the
atomistic scale. We find that high-energy radiation dam-
age creates unexpectedly large amount of damage. Im-
portantly, this damage is contained in point defects and
small clusters of point defects, and therefore does not
constitute what is usually considered as amorphization
in terms of the loss of long-range order, an insight that
arXiv:1307.3380v4[cond-mat.mtrl-sci]12Feb2014
3. 2
we additionally verify by direct calculation of the radial
distribution function. In contrast to the present results,
in some materials such as zirconium silicate (ZrSiO4) [24]
there is direct amorphization in the track and dense dam-
age is produced. In our simulations we find that the de-
fect atoms after the cascade relaxation represent dilute
damage. We briefly discuss the implications of our find-
ings for using zirconia as a waste form.
In this work, we perform MD simulations of radiation
damage in cubic zirconia due to high energies in the 0.1–
0.5 MeV range. To contain the damage due to these en-
ergies, we use system sizes with lengths of up to 130 nm
and 150 millions of atoms. We use the DL POLY pro-
gram, a general-purpose package designed for large-scale
simulations [25, 26]. The combination of nearly-perfect
scalability of the code with high–performance massive
parallel computer facilities has recently set the stage for
simulating systems of up to 1 billion atoms with realistic
interatomic potentials [27]. We have used the interatomic
potential that includes Buckingham pair interaction po-
tentials and partial Coulomb charges [28]. This poten-
tial stabilizes the cubic phase; we chose this potential to
study defect production in a cubic ceramic phase. Exper-
iments show [29] that there is no phase transformation or
grain restructuring during irradiation. Equilibrium U-O
interaction was the same as Zr-O interaction. The sys-
tem was equilibrated in the constant pressure ensemble
at 300 K. U atom with 0.1 MeV energy was chosen as
a primary recoil atom to correspond to the alpha-decay
process. Higher velocities of U atoms of the range of 0.3–
0.5 MeV correspond to heavy ion bombardment events.
The initial position of the U atom is 30-50 ˚A from the
simulation box boundaries. The propagation of the recoil
was followed in the constant energy and volume ensemble
when there is no energy loss. When the electronic stop-
ping mechanism in activated a friction term is included in
the equation of motion. We are using variable timestep
to account for faster atomic motion at the beginning of
the cascade development and its gradual slowing down at
later stages. To account for the highly non-equilibrium
nature of radiation damage, the following modifications
to the standard MD code were made. First, the MD box
boundary layer of thickness of about 10 ˚A was connected
to a Langevin thermostat at 300 K to emulate the effect
of energy dissipation into the sample. Second, we have
accounted for the electronic energy losses, particularly
important at high energies, by implementing the friction-
type term in the equations of motion applied to particles
above the certain cutoff energy Ec (or velocity) [30, 31].
In metals, Ec is often taken as approximately the double
of the system’s cohesion energy in order to differentiate
ballistically moving atoms (with energy in excess of cohe-
sion energy) from those oscillating. In insulators, it has
been shown that the band gap governs the electronic en-
ergy losses during the radiation damage process [32, 33],
and we have accordingly set Ec at twice the band gap
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
0 . 1 M e V 0 . 1 M e V
0 . 1 M e V 0 . 1 M e V
t [ p s ]
t [ p s ]
N d e f
N d i s p
t [ p s ]
N d e f
N d i s p
t [ p s ]
FIG. 1: Ndisp and Ndef (Ndef = Nint + Nvac) from 0.1 MeV
knock-on atoms without (top)and 0.1 MeV knock-on atoms
with the effect of electronic energy loss switched on (bottom)
for three directions of the recoil.
in zirconia. The friction coefficient was calculation us-
ing SRIM tables [34]. Finally, the Buckingham potential
was joined to a repulsive ZBL potential [35] at short dis-
tances using a switching function [36]. ZBL repulsion was
also used for all pair interactions. The simulations were
run on 3200–65000 parallel processors of UK’s National
Supercomputing Facilities, HECToR.
We have simulated recoils of 0.1, 0.3 and 0.5 MeV en-
ergies. Here, 0.1 MeV simulations are related to the re-
coil energy in Pu doping experiments where most of the
structural damage comes from heavy recoils with approx-
imately 0.1 MeV energy, whereas higher-energy events
correspond to heavy ion bombardment experiments. We
have simulated 0.1 MeV events with and without elec-
tronic energy loss whereas for higher energy events where
a significant part of energy loss is due to electronic pro-
cesses, the friction component was always on. For each
simulation, we have simulated three randomly chosen
directions of the recoil. The damage quantified below
therefore refers to the average numbers and includes the
standard deviation for each energy.
We quantify damage production, evolution and recov-
ery, and show the results in Figures 1-2. We introduce
two important quantities to describe the damage creation
and recovery: Ndisp and Ndef . Ndisp accounts for the to-
tal displacements introduced in the system, i.e. is the
number of atoms that have moved more than a cut–off
distance (d = 0.75 ˚A) from their initial positions. To
account for the atoms that recombine to crystalline po-
sitions, Ndef is introduced. Ndef reflects the recovery of
structural damage as it corresponds to the sum of inter-
stitials and vacancies. We use the sphere criterion for
defect identification [37]). If a particle, p, is located in
the vicinity of a site, s, defined by a sphere with its center
at this site and a radius, d, then the particle is a first-
hand claimee of s, and the site is not vacant. Otherwise,
the site is presumed vacant and the particle is presumed
4. 3
PEAK END
PKA energy Ndisp Nint (same for Nvac) Ndisp Nint (same for Nvac)
100 keV - no friction 104,000 (32,000) 96,000 (36,000) 8,000 (800) 750 (20)
100 keV - friction 72,000 (25,000) 70,000 (26,000) 6,000 (300) 600 (10)
300 keV - friction 113,000 (60,000) 105,000 (58,000) 14,000 (1,000) 1,600 (20)
500 keV - friction 230,000 (108,000) 220,000 (107,000) 22,000 (2,000) 2,600 (100)
TABLE I: Ndisp and Nint (Nvac), calculated using the sphere criterion, at the peak of the damage (1-2 ps) and at the end of
the simulation. Standard error of the mean is shown in the brackets calculated over three events.
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
1 0
6
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
1 0
6
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
0 . 1 1 1 0 1 0 0
1 0
3
1 0
4
1 0
5
N d e f
t [ p s ]
0 . 5 M e V
0 . 3 M e V
N d i s p
t [ p s ]
0 . 5 M e V
N d i s p
t [ p s ]
0 . 3 M e V
N d e f
t [ p s ]
FIG. 2: Ndisp and Ndef (Ndef = Nint + Nvac) from 0.3 MeV
knock-on atoms (top) and 0.5 MeV knock-on atoms (bottom)
for three directions of the recoil.
a general interstitial. If a site, s, is claimed and another
particle, p , is located within the sphere around it, then p
becomes an interstitial associated with s. After all par-
ticles and all sites are considered, it is clear which sites
are vacancies. Finally, for every claimed site, distances
between the site and its first hand claimee and intersti-
tials are compared and the particle with the shortest one
becomes the real claimee. If a first-hand claimee of s is
not the real claimee it becomes an interstitial associated
with s. At this stage it is clear which particles are inter-
stitials. The sum of interstitials and vacancies gives the
total number of defects in the simulated MD cell [38]. d
should generally be smaller than half of the closest inter-
atomic separation, and is usually chosen not to account
for typical thermal fluctuations of 0.2–0.3 ˚A. With a cer-
tain choice of d, Ndisp and Ndef can be compared and
agree with other methods of defect identification such as
Wigner-Seitz analysis [37, 39].
Fig. 1 shows Ndisp and Ndef for 100 keV cascades
along three different knock–on directions, without (top)
and with (bottom) the friction term. Fig. 2 illustrates
Ndisp and Ndef for 300 keV (top) and 500 keV (bottom)
cascades for the same directions of the U recoil atom.
We observe large peaks of both Ndisp and Ndef for all
simulated cascades, followed by the marked decrease and
saturation after about 5–10 ps of simulation time. Peak
and final, long-time, values of Ndisp and number of in-
terstitials (vacancies) Nint (Nvac) are summarized in Ta-
ble I. We observe a substantial effect of the electronic
friction on both Ndisp and Ndef , seen as a marked re-
duction of these numbers when the electronic friction is
on. This effect originates from smaller energy available
to produce both displaced atoms and surviving defects in
the presence of electronic energy loss, and demonstrates
the need to include electronic energy loss mechanisms in
high-energy radiation damage simulations. We observe
that the values of Ndisp and Ndef both at the peak and
at the end of the cascade increase with increasing energy.
Interestingly, we observed double peaks for cascades of
100 keV and 300 keV, which disappear for the higher en-
ergy cascades. This corresponds to the creation of sub-
cascades for the lower energy cascades and more contin-
uous damage morphology for the higher energy cascades
[27].
The physical origin of the large peaks is related to the
deformation of the crystalline lattice around the collision
cascade due to potential anharmonicity and associated
expansion of the cascade structure, and was discussed in
detail in our previous paper [27]. Here, we focus on the
final values of Ndisp and Ndef at long times, and the latter
in particular since it constitutes the remaining damage
after the cascade relaxation. As far as long-term evolu-
tion is concerned, experiments of irradiated zirconia [29]
show that with time and temperature, defect density de-
creases due to annihilation at sinks. Therefore, the pri-
mary damage state is the starting point to describe the
evolution of the microstructure.
First, we observe large dynamic recovery of the induced
damage, seen as the reduction of the final long-time Ndef
relative to Ndisp in Figures 1-2. The dynamic annealing
is profound, and constitutes 80%–99% of damage recov-
ery for different energies. This is consistent with earlier
simulations of smaller 30 keV energy [39], and is well il-
lustrated in Fig. 3 where we show both displaced and
defect atoms for each simulated energy at various stages
of damage propagation. In this figure, a typical cascade
size, the maximal distance between defect atoms at the
end of cascade propagation, is 600–1200 ˚A. In 8 out of
the 12 cascade simulations the U recoil is not identified
as a ”defect”.
Fig.4 shows displaced and defect atoms in a 300 keV
cascade at different time frames, which corresponds to
the middle line (double-peak) shown in the top plots of
5. 4
Fig.2. In contrast to the cascade shown in Fig.3(b), which
shows continuous shape of the damage and corresponds
to the single peak line of Fig.2, we see a resolvable smaller
subcascade at the bottom. These two pockets expand
and relax with time difference of about 2.5 ps. The first
frame is at 1.4 ps where the bottom subcascade reaches
its maximal size, corresponding to the first peak shown
in Fig.2. In the second frame (2.5 ps) the smaller pocket
reduces in size, followed by the larger pocket (left top
corner) reaching its maximal size at 4.1 ps in the third
frame. This is confirmed by counting the atoms in both
subcascades at different times. The dilute damage on the
right of the cascade in Fig. 4 is due to channelling in this
event.
The key to reconciling the exceptional radiation toler-
ance of ZrO2 on experimental basis and the large number
of defect atoms comes from realization that the dam-
age at the end of the simulation time is very dilute, and
mostly consists of isolated point defects and small disjoint
clusters. In this case, X-ray probes, TEM and other non-
local experimental probes do not detect amorphization as
the loss of the long–range order, and hence consider zir-
conia as highly resistant despite the presence of the large
number of local defects.
First, we support our proposal by the detailed analysis
of defect atoms and the cascade morphology. In Table
II, we summarize how Ndef partition in clusters of dif-
ferent sizes. As discussed later, we find that across all
cascades simulated, the majority of the defects are iso-
lated, most of which are O vacancies. In Fig. 5, we show
the distribution of cluster sizes, and similarly find that
most of the damage resides in isolated point defects and
small clusters. Notably, we find that vacancy clusters to
be appreciably larger than interstitial clusters (see Table
II and Fig. 5), the point to which we return below.
Second, we calculate the radial distribution function
(RDF) over atoms in four simulated collision cascades.
We define the radius of gyration of the collision cas-
cade as RG = ∆r/N, where ∆r is the distance be-
tween interstitials and the centre of gyration. We cal-
culate RDF as a histogram of separations between all
atoms located within the sphere of radius RG centered
at rC = ri/N, where ri are positions of identified in-
terstitial defect atoms i and N is their number. In Fig.
6 we show t(r) = g(r) · r, where g(r) is normalized to
the value 1 for large distances, calculated for the crys-
talline structure and the difference of t(r) between the
crystalline structure and four collision cascades. Fig.
6 shows the near-identity of RDFs between the dam-
aged and crystalline structure including, importantly, the
presence of peaks beyond the short- and medium-range
order. This is in contrast to the disappearance of peaks
beyond the medium-range order in systems such as SiO2,
TiO2, ZrSiO4 and so on where in-cascade amorphization
is observed [24, 40–42].
We now give more details about the nature of radiation
FIG. 3: Time frames of displaced and defect atoms for differ-
ent recoil energy cascades with the effect of electronic energy
loss switched on. The knock-on atom moves from the top left
to the bottom right corner. Oxygen atoms are represented in
red and zirconium atoms in gray. Top images represent the
displaced atoms and the bottom images the defect atoms.(a)
0.1 ps, 1.1 ps and 50 ps in a 0.1 MeV collision cascade in a
system with box length of 645 ˚A, consisting of about 20 mil-
lion atoms. Cascade size (maximal separation between any
two defect atoms in the cascade) is about 600 ˚A. (b) 0.1 ps,
0.45 ps and 64 ps for a collision cascade of 0.3 MeV collision
cascade in a 70 million atoms system with box length of about
1000 ˚A. Cascade size is 800 ˚A. (c) 0.1 ps, 1.2 ps and 17 ps
for a 0.5 MeV collision cascade in a system of about 1300 ˚A
length, consisting of 150 million atoms. Cascade size is 1200
˚A.
6. 5
1.4 ps
125,000 defect atoms
2.5 ps
50,000 defect atoms
4.1 ps
130,000 defect atoms
2.5 ps
35,000 displaced atoms
4.1 ps
75,000 displaced atoms
1.4 ps
70,000 displaced atoms
FIG. 4: Time frames of displaced and defect atoms for a
300 keV cascade where the effect of electronic energy loss is
switched on. The knock-on atom moves from the top left to
the bottom right corner. Oxygen atoms are represented in red
and zirconium atoms in gray. The three frames shown are at
1.4 ps, 2.5 ps and 4.1 ps and correspond to the first peak, the
following minimum and the second peak of the double-peak
plot in the top of Fig.2. The system consists of about 70
million atoms and has box length of about 1000 ˚A. Cascade
size is about 800 ˚A. The smaller pocket of damage reaches its
maximal size and relaxes faster than the larger one on the top
left corner of the simulation box.
FIG. 5: Distribution of cluster sizes for all cascades per-
formed.
damage in ZrO2 presented in Table II. We perform the
analysis excluding vacancy-interstitial (V-I) pairs of the
same species (both cation or both O) that lie within 3 ˚A
of each other under the assumption that they will quickly
annihilate with each other. We define clusters based on
defects being within 3 ˚A of a defect, i.e for vacancy -
vacancy (V-V) distance and interstitial - interstitial (I-I)
distance less 3 than ˚A. The number of surviving defects
increases with increasing energy with an almost linear
FIG. 6: t(r) calculated for the crystalline system and the
differences between t(r) for the crystalline structure and t(r)
for the damaged structures for four collision cascades.
dependence. Our numbers of interstitials as a function
of energy for the friction case give an exponent of about
0.9. If n is the number of interstitials and E is the PKA
energy, then according to our data (n1/n2) = (E1/E2)0.9
.
The defect production in previous work in metals and
ceramics in simulations of PKA energy up to 150 keV [44,
45], where the electronic effects have not been taken into
account, shows linear dependence on the PKA energy.
The longest separation between defects in the cascade
increases with increasing energy and is also larger if no
friction is applied, reflecting that including electronic
stopping in high energy cascades results in smaller cas-
cade size. This is also demonstrated by the radius of gy-
ration at the end of the cascades, with values of 53, 91,
141, 210 ˚A averaged over three events for 100 keV cas-
cades with electronic stopping, 100 keV cascades without
the friction term applied, 300 keV and 500 keV cascades
respectively. There is no obvious trend in the average
distance between vacancies and nearest interstitials on
the same sublattice with increasing energy or inclusion
of friction. However, the Zr V-I separation is slightly
larger than the O V-I separation, with the standard de-
viation of this distance being larger for the O sublattice.
Therefore O defects can be found with large V-I sepa-
rations. The fraction of vacancies and interstitials that
are associated with the anion sublattice is 0.71 to 0.74
regardless of energy or friction. 30-38% of vacancies are
isolated and this percent does not vary significantly with
energy or friction. 44-49% of interstitials are isolated and
again there is not much variation with energy or friction.
Interstitials are more likely to be isolated than vacancies.
Roughly one half of interstitials and on third of vacancies
are isolated.
Consistent with the above, interstitial cluster sizes are
smaller than vacancy cluster sizes. The largest interstitial
7. 6
cluster, consisting of both Zr and O, size is consistently
between 3 and 4 regardless of energy or friction. Vacancy
clusters are larger and the size of the largest cluster in-
creases with energy and also if friction is ignored. The
largest vacancy cluster is between 11 and 21 vacancies.
These vacancy clusters are either 50% O (Zr-O clusters)
or fairly close to the stoichiometric ratio (O-Zr-O vacancy
clusters). Fraction of oxygen among isolated vacancies
is 0.92 to 0.94 and among isolated interstitials is 0.95
to 0.97. This seems independent of the energy and elec-
tronic stopping effect. Isolated defects are predominantly
(almost entirely) on the oxygen sublattice.
We have brought insight into the primary damage
state, by going beyond previous work in taking the elec-
tronic effects into account through the friction term. This
information can serve as input for mesoscale models that
incorporate grain boundaries and sinks and propagate
the system much farther in time than possible with MD
simulations. The results of such modeling can be directly
compared to experiments and will be the subject of fu-
ture study. Even though zirconia does not amorphize in
a sense of losing long-range order as most of the systems
do [24], a large number of point defects and their clus-
ters found here may play an important role in long-term
evolution of the damage [46] and increased diffusion of ra-
dioactive species in particular. Especially relevant in this
context is the larger size of the vacancy clusters (9–21, see
Table II and Fig. 5) as compared to the size of interstitial
clusters (3–5, see Table II and Fig. 5). Consistent with
experimental results [8, 12–14], these can provide fast dif-
fusion pathways for encapsulated radioactive species, but
also play a role in the nucleation and growth of bubbles
affecting the overall performance of the waste form. Ex-
periments also show that defect clusters can also serve
as sinks for point defects [29]. Similar effects can be rel-
evant in materials such as the widely used nuclear fuels
UO2 that are similar to zirconia in terms of structure and
bonding.
In summary, we have found that a large number of
point defects and their clusters co-exist with long-range
structural coherence in irradiated zirconia. These de-
fect structures are largely disjoint from each other and
therefore represent a dilute damage that does not result
in the loss of long-range structural coherence and amor-
phization. At the same time, long-time evolution of these
defects may have important implications for using zirco-
nia in intense radiation environments.
This work made use of the facilities of HECToR, via
the Materials Chemistry Consortium, funded by EPSRC
(EP/F067496). RD and WJW were supported by the
U.S. Department of Energy, Office of Basic Energy Sci-
ences, Division of Materials Sciences and Engineering.
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9. 8
Property Cascade 100keV fr 100keV no fr 300keV 500keV
Surviving Zr vac 1 103 141 252 390
(same for Zr int) 2 105 117 257 465
3 103 123 269 391
Surviving O vac 1 242 338 742 1105
(same for O int) 2 266 310 741 1219
3 257 357 759 1035
Surviving defects 1 690 958 1988 2990
(vac and int of Zr and O) 2 742 854 1996 3368
3 720 960 2056 2852
Longest distance 1 585.88 453.90 830.57 1177.85
between defects (˚A) 2 380.08 440.39 1055.44 1262.62
3 365.01 559.40 1019.81 1240.10
Zr int-vac distance (˚A) 1 12.68 12.66 12.23 12.02
2 12.07 12.35 11.69 12.37
3 12.84 11.93 12.29 12.14
O int-vac distance (˚A) 1 12.25 11.31 10.30 10.41
2 11.16 10.82 10.47 10.86
3 11.33 10.91 10.39 10.83
Fraction of O vac 1 0.70 0.71 0.75 0.74
2 0.72 0.73 0.74 0.72
3 0.71 0.74 0.74 0.73
Fraction of O int 1 0.70 0.71 0.75 0.74
2 0.72 0.73 0.74 0.72
3 0.72 0.74 0.74 0.73
Fraction isolated vac 1 0.26 0.26 0.38 0.36
2 0.33 0.30 0.38 0.32
3 0.32 0.36 0.38 0.36
Fraction isolated int 1 0.42 0.42 0.50 0.48
2 0.46 0.44 0.49 0.47
3 0.45 0.50 0.48 0.47
Frac O in isolated vac 1 0.91 0.94 0.96 0.95
2 0.91 0.92 0.94 0.94
3 0.93 0.94 0.93 0.92
Frac O in isolated int 1 0.96 0.95 0.96 0.97
2 0.94 0.98 0.97 0.95
3 0.96 0.96 0.97 0.95
Size of largest vac cluster 1 11 13 12 14
2 9 9 12 17
3 14 21 11 14
Size of largest int cluster 1 5 3 3 3
2 3 4 3 4
3 3 3 4 3
TABLE II: Defect analysis for different recoil energy cascades, for three different directions of the recoil. fr stands for friction,
vac for vacancies, int for interstitials
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