On the Use of Chromium Coating for Inner-Side Fuel Cladding Protection: Thickness Identiﬁcation Based on Fission Fragments Implantation and Damage Proﬁle

: Inner-side coatings have been proposed as a complementary solution within the accident tolerant fuel (ATF) framework, to provide enhanced protection for the nuclear fuel cladding. Unlike external surface, the degradation of irradiated internal cladding surface has not been studied extensively. Fission fragments produced during the ﬁssion of nuclear fuel is one of the key players in this degradation. This study aimed to estimate the minimum thickness of the thin chromium ﬁlm, required to protect the inner side of the nuclear fuel cladding. The approach used is based on a set of calculations, of Ion ranges and damage proﬁles, for a group ﬁssion fragments, using the TRIM code. The calculation results were veriﬁed by comparison with the experimental data associated with the phenomena of the inner cladding degradation of thermo-releasing elements. The recommended minimum thickness for such a ﬁlm was found to be 9 microns. Calculations also showed that chromium metal has a greater stopping power compared to the zirconium-based alloy E110, which indicates an increased ability of chromium to withstand exposure to energetic ﬁssion fragments during reactor operation.


Introduction
As a response to the design flaws exposed by Fukushima Nuclear Accident in 2011, a global shift has been occurred in nuclear fuel research, towards a fuel with specific ability to tolerate accidents.The concept of accident-tolerant fuel (ATF) has emerged as a unique fuel design expected to improve the safety of nuclear reactors.The underlying principle behind the ATF concept is to enable a reactor core to remain intact for a rather long time without the need for swift operator interventions in cases of severe events, when the external cooling supply is lost.Among the core tasks of ATF, is the design of cladding materials with outstanding performance [1].
Numerous cladding concepts have been proposed, however; those involving a complete replacement for the zirconium based alloys have a greater uncertainty and would represent a relatively long-term solutions.In contrast, using protective surface coatings with the existing zirconium alloys is expected to provide improved performance, without introducing significant changes into the current uranium dioxide -zirconium (UO 2 -Zr) fuel system design.This would represent a more conservative, short-term technical route with favorable application prospects [1].
Due to its high melting point, intrinsic ductility and similar thermal expansion coefficient to that of zirconium (Zr) [1,2], Metallic chromium (Cr) has attracted attention as a potential coating material on zirconium alloys, to limit external cladding corrosion in normal operating conditions, and to delay zirconium oxidation during severe accidents events.An extensive research has been triggered worldwide to investigate the feasibility of Coatings 2021, 11, 710 2 of 16 this solution.Different deposition technologies haves been used, such as: physical vapor deposition (PVD) by CEA (France), vacuum arc ion-plasma technology in Russia, 3D laser technology, cold spraying and arc ion plating in Korea [2].This research showed that applying metallic chromium thin film significantly improved corrosion resistance in Zircaloy claddings [3,4].Coated samples demonstrated negligible reduction in residual strength and ductility, improved ballooning and rapture resistance, and reduced hydrogen pickup, compared with uncoated Zircaloy claddings in light water reactors (LWRs) environment.This further enhances life extension and burnup efficiency of nuclear fuel [1], however; research focused mainly on depositing chromium coating on the external surface of cladding.A realistic scenario that steam from the outer environment enters the cladding tube, through a rupture after ballooning and bursts, under loss of coolant accident (LOCA) conditions, or through cracks arise as a consequence to stress corrosion cracking (SCC) phenomenon, led by the projected stresses on the deformed fuel and the presence of accumulated fission products (FPs) in the pellet-clad interface (PCI).Steam leaked into the unprotected inner surface of cladding can cause a rapid oxidation and secondary hydrogenation, eventually complicating the accident scenario further [1].
Unlike external surface, the oxidation and degradation of the irradiated internal surface of fuel cladding have not been studied extensively.The presence of fission fragments produced by the fission of nuclear fuel has been closely linked to this degradation.Indeed, the contribution of FPs to the damage of fuel cladding materials has been known for a long time.During a reactor's operation, the dose rate of FPs is approximately 12.5 times to that of neutron and gamma radiation [5].Phenomena such as corrosion, SCC, embrittlement and reduction of ductility [6,7] has been closely linked to the aggressive environment caused by the presence of FPs and their migration to the internal surface of the cladding.
To provide protection and limit the damage on the internal side of fuel cladding, applying an inner thin film coating have been proposed [8].In fact; this concept is not new, internal surface coatings were proposed in the 1970s as a solution for the problem of SCC in power reactors.A graphite film successfully applied in CANDU reactor claddings due to its relatively short length (about 0.5 m), however; obstacles such as the practicality of applying thin films on the internal wall of a 4.5 m long tube has hindered the wide implementation of this solution [9].Recently; the advancements in thin film technologies brought this topic into the front as a complementary solution within the ATF framework [8,10,11], nevertheless; there are still several process parameters which need to optimized such as coating's structure, defects, and thickness.
As an attempt to bring some new comprehension elements that would contribute in optimizing surface coating process parameters, this study aims to identify the minimum Chromium thin film thickness, which is able to provide sufficient protection for the internal surface of fuel cladding.The approach used, is based on identifying the potential extension of internal damage, through set of calculations, of the maximum implantation depths and damage profiles for a group of FPs, mostly known to have major contributions in the degradation of the internal surface of fuel cladding.Based on this calculations; a minimum thin film thickness is selected.This film is expected to offer a substantial degree of protection, by containing and limit the effects of FPs migrating to fuel cladding walls.Furthermore, this established approach could be beneficial in indentifying the minimum inner-surface thin film thickness, for various coating materials proposed within the ATF framework, based on the material being investigated.

Fission Products
Ion ranges and displacement damage was simulated for a group of FPs using TRIM-2008, to identify the maximum implantation ranges and damage profiles for this FPs inside the internal surface of fuel cladding.The group of FPs included: noble metal phase particles: technetium (Tc), ruthenium (Ru), molybdenum (Mo), rhodium (Rh) and palladium (Pd), in addition to the volatile products iodine (I), and cesium (Cs).The Zr-based alloy E110 (composition is given in Table 1), widely utilized as fuel cladding material in Russian WWER reactors, was used as a substrate in this simulation.Based on the calculated ranges and damage; an appropriate thin film thickness of metalic Cr was designated.Based on the experimental measurements, fission fragments are produced with different energies and different yields [12,13].The more energetic the particle, the more it can travel inside the material.As a conservative approach, the maximum expected energies, which is normally corresponds to very small yields [12], is used in the simulations performed in this study, this will contribute to a more precise selection of the minimum thickness of thin film.
The simulated FPs is characterized by the relatively high production yield during nuclear fuel fission process.Traces of these products have been detected inside the fuel cladding by many researchers, and a close linkage were firmly established between their presence and many cladding degradation phenomena, such as the internal corrosion, the SCC, the internal cladding surface hardening, embrittlement and reduction of ductility.Experimental observations showed that the noble metal phase particles exist as polycrystalline metallic agglomerates [14] inside the internal cladding wall, this marks these products as key players in cracks initiation [15], due to the consequent hardening caused by their presence in this form.Once cracks is initiated, Corrosive volatile species; such as iodine and cesium find their way through the cracks, react with zirconium, and cause further corrosion, eventually extending this cracks through the cladding walls.
Different initial numbers of incident ions were simulated, e.g., 4000, 10,000, 20,000, 30,000, etc.The simulations showed that the range of this ions and the damage seem to be saturated (cascade saturation) after a certain number of ions, as the calculated ranges and damage gave the same implantation depths, and almost the same damage for the different number of incident ions.The number of incident ions for the simulated group of FPs is taken to be 4000 ions in this study.

SRIM Software
Stopping and Range of Ions in Matter (SRIM) is a software package developed by Ziegler (Rockville, MD, USA), based on the binary collision approximation (BCA) method [16].It has the ability to estimate many features related to the transport of ions in matter [13,16,17].The BCA is a Monte Carlo method designed to calculate deposition profiles in materials exposed to energetic ion beams.The underlying assumption is that an energetic particle collides with a target atoms will lose its kinetic energy in this collosions, elasticly with atoms, and inelasticly with electrons, target atoms may receive enough energy to undergo additional collisions.
Transport of Ions in Matter (TRIM) is one of SRIM modules, widely used in ion beam implantation and processing calculations [17], it accepts and handles complex targets (compound materials) with many layers up to eight.TRIM offers different options to estimate the damage in a target, based on the type and details of outputs required.The full damage cascade (F-C) mode follows each recoiling atom (primary, secondary, etc), until its energy drops below threshold displacement energy (E d ) of any target atom, therefore, all collisions to the target is considered and analyzed.The quick calculation of damage (K-P) mode follows only the path of incidence ions, it could be used when little attention is needed about the details of the target damage or the surface sputtering.The calculated damage with this option represents a quick statistical estimate based on the Kinchin-Pease formalism "K-P" [18].Both F-C and K-P options give the same ion ranges in a specific target [12], however; the first method is time consuming when compared with the K-P method since the progression of the cascade is not followed in the later.As we are mainly interested in the range of ions and the depth of the damage rather than the damage details, the second method have been adopted in this study.
K-P theory is originally proposed by Kinchin and Pease, extended by Lindhard, and later by Norgett, Robinson and Torrens (NRT)] [16].In this theory, the defect producing energy E ν , is obtained from the transferred energy T of the recoil by taking into account electronic losses [16]: where the electronic losses are governed by: where Z 2 and M 2 are the atomic number and atomic mass for the target atoms and: where ε d is a reduced energy given by: From the transferred energy to target atoms, E ν, the number of displacements, ν, is calculated by the modified Kinchin-Pease model: TRIM inputs used in this study are given in Table 2.The displacement energy is the energy required by a recoil atom, to overcome the lattice forces, and to move more than one atomic spacing away from its original site.The lattice binding energy is the energy that every target atom loses, when it leaves its lattice site and recoils in the target, and the Surface binding energy is the energy that target atoms must overcome to leave the surface of the target.

Ion Ranges
Figures 1 and 2 show the calculated ion ranges for the noble metal phase particles: Tc, Ru, Mo, Rh, and Pd, in addition to volatile products iodine and Cs, in the zirconium based alloy E110.This corresponds to the maximum recoil energy for these elements from the fission of uranium -235 (U 235 ).The fission yield for this group of products, which is expected to reach the inner surface of the fuel cladding with such high recoil energies, is anticipated to be very small.According to calculations made by Rymzhanov et al. [12], in an attempt to estimate the relative yield, energy and flux of fission fragments (from the fission of 235 U and plutonium 239 Pu) on the surface of nuclear fuel cladding, using the experimental spectra of fission products, this yield is expected to range between 10 −8 to 10 −9 .This extremely small yield is probably the reason behind the inability to experimentally detect the physical presence of these products behind certain depths inside fuel cladding in some studies, such as those done in [5,14].As these particles are being ejected with very high levels of energy, the damage caused was actually recorded in depths higher than that in which their physical presence was confirmed by Lach et al. [5].Nevertheless, the small and very limited yield may have inhibited the agglomeration of these particles, and thus, impeding their physical detection by some researchers.
As shown in Figures 1 and 2, the depths into which those elements could reach inside the fuel cladding ranges between ~8-10 µm.This result is fairly consistent with the findings of Hirabayashi et al. [19], in their investigation of the distribution of radionuclides in PWR spent fuel Zircaloy-4 cladding, using a stepwise etching process.According to these findings, more than 98% of fission products in the cladding exist within a 10 µm depth from the inner surface of the cladding.Moreover, the abundance of fission products inside the cladding have shown to follow a gradient distribution with the depth, this could be directly linked to the gradient in yield and energy for fission recoils reaching the inner surface of fuel cladding [12].
based alloy E110.This corresponds to the maximum recoil energy for these elements from the fission of uranium -235 (U 235 ).The fission yield for this group of products, which is expected to reach the inner surface of the fuel cladding with such high recoil energies, is anticipated to be very small.According to calculations made by Rymzhanov et al. [12], in an attempt to estimate the relative yield, energy and flux of fission fragments (from the fission of 235 U and plutonium 239 Pu) on the surface of nuclear fuel cladding, using the experimental spectra of fission products, this yield is expected to range between 10 −8 to 10 −9 .This extremely small yield is probably the reason behind the inability to experimentally detect the physical presence of these products behind certain depths inside fuel cladding in some studies, such as those done in [5,14].As these particles are being ejected with very high levels of energy, the damage caused was actually recorded in depths higher than that in which their physical presence was confirmed by Lach et al. [5].Nevertheless, the small and very limited yield may have inhibited the agglomeration of these particles, and thus, impeding their physical detection by some researchers.
As shown in Figures 1 and 2, the depths into which those elements could reach inside the fuel cladding ranges between ~ 8-10 µm.This result is fairly consistent with the findings of Hirabayashi et al. [19], in their investigation of the distribution of radionuclides in PWR spent fuel Zircaloy-4 cladding, using a stepwise etching process.According to these findings, more than 98% of fission products in the cladding exist within a 10 µm depth from the inner surface of the cladding.Moreover, the abundance of fission products inside the cladding have shown to follow a gradient distribution with the depth, this could be directly linked to the gradient in yield and energy for fission recoils reaching the inner surface of fuel cladding [12].The results obtained in Figures 1 and 2 are also similar to the observations made by Ciszak et al. [20] in their study of the fuel-cladding bonding layer in high burnup fuel for a sample prepared from a Zircaloy-4 cladded fuel rod, and examined using micro-Raman spectroscopy.They demonstrated an implantation gradient of the fission products on the zirconia scale, these FPs implantations ranged from 8 to 10 µm in depth inside the zirconia.
The implantation ranges for Pd, Ru and Rh particles with lower recoil energies (produced in a higher yield during the fission process ~ 5 × 10 −4 -10 −5 [12]) was also simulated (Figure 3), to show that these particles would own shorter ranges inside the zirconium based cladding.In this case, since the yield is higher, more atoms will be available to agglomerate and form the polycrystalline particles observed by T.G.Lach et al. [5], in their investigation of the effects of FPs metal particles, on the stability and grain size of the tetragonal phase Zirconium-oxide (ZrO2), forms in BWR fuel cladding liner at high burnup.In this study, the authors have detected the presence of solid noble metal particles (Mo, Tc, Ru, Rh, and Pd) in depths between 5.5-6 µm inside the ZrO2, which coincides with the same depth at which the pure ZrO2 tetragonal phase occurs.Beyond this region of a purely tetragonal phase, they observed a transition region that consists of a combination of both tetragonal and monoclinic phases, but no fission particles was detected.The authors attributed this to the presence of fission recoil radiation at a rate high enough to partially stabilize the tetragonal phase, but too low to accumulate atoms into particles.
The results obtained in Figure 3 also show a good agreement with the study of Clark et al. [14], in which they performed a detailed microscopic analysis for fission products in the cladding.They detected the presence of noble metal phase particles (Tc, Ru, Mo, Rh and Pd) in a form of agglomerated polycrystalline particles, rather than single crystals form, within the oxidized phase of Zr liner of spent nuclear fuel.The morphology and size distribution of the noble metal phase particles varied as a function of depth from the UO2 fuel to the Zr-oxide region.Within the first 3-4 µm from the fuel, there were large particles with diameters greater than 100 nm coexisting with particles that were about 50 -70 nm in diameter.As the depth into the Zr-oxide increased up to 5-6 µm, the average size of the particles decreased.The findings in [14] again confirm the assumption that FPs follow a gradient distribution in yield and energy, in their migration from the fuel into the inside surface of the cladding, the higher the energy; the lower the yield, and the longer the depth a fission recoil will reach inside the fuel cladding.Within shorter depths, as the yield is higher, more atoms were available to agglomerate and form the large particles observed The results obtained in Figures 1 and 2 are also similar to the observations made by Ciszak et al. [20] in their study of the fuel-cladding bonding layer in high burnup fuel for a sample prepared from a Zircaloy-4 cladded fuel rod, and examined using micro-Raman spectroscopy.They demonstrated an implantation gradient of the fission products on the zirconia scale, these FPs implantations ranged from 8 to 10 µm in depth inside the zirconia.
The implantation ranges for Pd, Ru and Rh particles with lower recoil energies (produced in a higher yield during the fission process ~5 × 10 −4 -10 −5 [12]) was also simulated (Figure 3), to show that these particles would own shorter ranges inside the zirconium based cladding.In this case, since the yield is higher, more atoms will be available to agglomerate and form the polycrystalline particles observed by T.G.Lach et al. [5], in their investigation of the effects of FPs metal particles, on the stability and grain size of the tetragonal phase Zirconium-oxide (ZrO 2 ), forms in BWR fuel cladding liner at high burnup.In this study, the authors have detected the presence of solid noble metal particles (Mo, Tc, Ru, Rh, and Pd) in depths between 5.5-6 µm inside the ZrO 2 , which coincides with the same depth at which the pure ZrO 2 tetragonal phase occurs.Beyond this region of a purely tetragonal phase, they observed a transition region that consists of a combination of both tetragonal and monoclinic phases, but no fission particles was detected.The authors attributed this to the presence of fission recoil radiation at a rate high enough to partially stabilize the tetragonal phase, but too low to accumulate atoms into particles.
The results obtained in Figure 3 also show a good agreement with the study of Clark et al. [14], in which they performed a detailed microscopic analysis for fission products in the cladding.They detected the presence of noble metal phase particles (Tc, Ru, Mo, Rh and Pd) in a form of agglomerated polycrystalline particles, rather than single crystals form, within the oxidized phase of Zr liner of spent nuclear fuel.The morphology and size distribution of the noble metal phase particles varied as a function of depth from the UO 2 fuel to the Zr-oxide region.Within the first 3-4 µm from the fuel, there were large particles with diameters greater than 100 nm coexisting with particles that were about 50-70 nm in diameter.As the depth into the Zr-oxide increased up to 5-6 µm, the average size of the particles decreased.The findings in [14] again confirm the assumption that FPs follow a gradient distribution in yield and energy, in their migration from the fuel into the inside surface of the cladding, the higher the energy; the lower the yield, and the longer the depth a fission recoil will reach inside the fuel cladding.Within shorter depths, as the yield is higher, more atoms were available to agglomerate and form the large particles observed by the authors in [14], as the depth increased, the yield decreased, therefore the average size of the particles decreased.

Damage Profiles and Thin Film Thickness.
The maximum damage in E110 alloy, which corresponds to maximum anticipated recoil energies for FPs, was simulated.Based on the implantation and damage ranges, a minimum thin film thickness that would be able to provide sufficient protection for the inner-surface of fuel cladding is selected.
Figure 4 shows the damage caused by 120 MeV Tc in E110, calculated by TRIM using Kinchin-Pease approximation.The damage extends to a depth of over 10 µm inside the cladding.A total damage of 27,162 vacancies per ion is produced in the alloy.A thin film of Cr of about 9 µm was applied and a simulation for the damage was done again.It has been found that this thickness will be suitable to provide protection for the cladding material, as it efficiently contained the damage of this energetic particle (Figure 5).Its worth mentioning that the total damage created by the same ion, with same energy, is much less when applying a chromium thin film as it is estimated to be 22,725 vacancies /ion.Since TRIM assumes that all targets are amorphous, this is cannot be explained in the context of crystallographic differences, however; this could be arising from the differences in atomic and electronic structures.

Damage Profiles and Thin Film Thickness
The maximum damage in E110 alloy, which corresponds to maximum anticipated recoil energies for FPs, was simulated.Based on the implantation and damage ranges, a minimum thin film thickness that would be able to provide sufficient protection for the inner-surface of fuel cladding is selected.
Figure 4 shows the damage caused by 120 MeV Tc in E110, calculated by TRIM using Kinchin-Pease approximation.The damage extends to a depth of over 10 µm inside the cladding.A total damage of 27,162 vacancies per ion is produced in the alloy.A thin film of Cr of about 9 µm was applied and a simulation for the damage was done again.It has been found that this thickness will be suitable to provide protection for the cladding material, as it efficiently contained the damage of this energetic particle (Figure 5).Its worth mentioning that the total damage created by the same ion, with same energy, is much less when applying a chromium thin film as it is estimated to be 22,725 vacancies /ion.Since TRIM assumes that all targets are amorphous, this is cannot be explained in the context of crystallographic differences, however; this could be arising from the differences in atomic and electronic structures.
by the authors in [14], as the depth increased, the yield decreased, therefore the average size of the particles decreased.

Damage Profiles and Thin Film Thickness.
The maximum damage in E110 alloy, which corresponds to maximum anticipated recoil energies for FPs, was simulated.Based on the implantation and damage ranges, a minimum thin film thickness that would be able to provide sufficient protection for the inner-surface of fuel cladding is selected.
Figure 4 shows the damage caused by 120 MeV Tc in E110, calculated by TRIM using Kinchin-Pease approximation.The damage extends to a depth of over 10 µm inside the cladding.A total damage of 27,162 vacancies per ion is produced in the alloy.A thin film of Cr of about 9 µm was applied and a simulation for the damage was done again.It has been found that this thickness will be suitable to provide protection for the cladding material, as it efficiently contained the damage of this energetic particle (Figure 5).Its worth mentioning that the total damage created by the same ion, with same energy, is much less when applying a chromium thin film as it is estimated to be 22,725 vacancies /ion.Since TRIM assumes that all targets are amorphous, this is cannot be explained in the context of crystallographic differences, however; this could be arising from the differences in atomic and electronic structures.It could be noticed that using 8 µm film of Cr would possibly contain the damage caused by the energetic Tc recoil, nevertheless; the range of Tc in metallic Cr is estimated to be 7.29 µm in this case (Figure 6).Thus, the damage may extend to the cladding/chromium coating interface region as shown in Figure 7, which in turn would possibly affect coating adhesion, as defects and vacancies will be existing near the interface region.It's also obvious from Figure 7 that the concentration of vacancies is the highest near the interface region; this may lead to creation of voids, as a result to the coexistence of large number of vacancies, which in turn would compromise the cohesion of the coating.It could be noticed that using 8 µm film of Cr would possibly contain the damage caused by the energetic Tc recoil, nevertheless; the range of Tc in metallic Cr is estimated to be 7.29 µm in this case (Figure 6).Thus, the damage may extend to the cladding/chromium coating interface region as shown in Figure 7, which in turn would possibly affect coating adhesion, as defects and vacancies will be existing near the interface region.It's also obvious from Figure 7 that the concentration of vacancies is the highest near the interface region; this may lead to creation of voids, as a result to the coexistence of large number of vacancies, which in turn would compromise the cohesion of the coating.It could be noticed that using 8 µm film of Cr would possibly contain the damage caused by the energetic Tc recoil, nevertheless; the range of Tc in metallic Cr is estimated to be 7.29 µm in this case (Figure 6).Thus, the damage may extend to the cladding/chromium coating interface region as shown in Figure 7, which in turn would possibly affect coating adhesion, as defects and vacancies will be existing near the interface region.It's also obvious from Figure 7 that the concentration of vacancies is the highest near the interface region; this may lead to creation of voids, as a result to the coexistence of large number of vacancies, which in turn would compromise the cohesion of the coating.Figure 8 shows the calculated maximum damage caused by ruthenium (Ru) fission product in the fuel cladding (E110).This corresponds to recoil energy of about 120 MeV.The calculations show that a thin film of Cr of about 9 µm will be able to protect the inner surface of fuel cladding from the effect of this FP (Figure 9).The difference in the calculated displacement damage could also be observed for this case.Note that no replacement collisions have been registered, this is because; replacement collisions occur when the incident ions and the target have the same atomic numbers, and the incident ion loses it energy to a target atom, the target atom gain enough energy to leave its lattice site, while the incident ion remains with no energy to induce further collisions, in this case, it replaces the target atom and fall into the vacancy site created by its movement.The other case for the occurrence of replacement collisions is in single element targets with large recoil cascades.Since the cascade propagation is not followed here, this type of collision will not occur.Figure 8 shows the calculated maximum damage caused by ruthenium (Ru) fission product in the fuel cladding (E110).This corresponds to recoil energy of about 120 MeV.The calculations show that a thin film of Cr of about 9 µm will be able to protect the inner surface of fuel cladding from the effect of this FP (Figure 9).The difference in the calculated displacement damage could also be observed for this case.Note that no replacement collisions have been registered, this is because; replacement collisions occur when the incident ions and the target have the same atomic numbers, and the incident ion loses it energy to a target atom, the target atom gain enough energy to leave its lattice site, while the incident ion remains with no energy to induce further collisions, in this case, it replaces the target atom and fall into the vacancy site created by its movement.The other case for the occurrence of replacement collisions is in single element targets with large recoil cascades.Since the cascade propagation is not followed here, this type of collision will not occur.Figure 8 shows the calculated maximum damage caused by ruthenium (Ru) fission product in the fuel cladding (E110).This corresponds to recoil energy of about 120 MeV.The calculations show that a thin film of Cr of about 9 µm will be able to protect the inner surface of fuel cladding from the effect of this FP (Figure 9).The difference in the calculated displacement damage could also be observed for this case.Note that no replacement collisions have been registered, this is because; replacement collisions occur when the incident ions and the target have the same atomic numbers, and the incident ion loses it energy to a target atom, the target atom gain enough energy to leave its lattice site, while the incident ion remains with no energy to induce further collisions, in this case, it replaces the target atom and fall into the vacancy site created by its movement.The other case for the occurrence of replacement collisions is in single element targets with large recoil cascades.Since the cascade propagation is not followed here, this type of collision will not occur.The maximum anticipated recoil energy for molybdenum (Mo) produced during the fission of nuclear fuel is about 120 MeV.This high energetic particle is expected to induce a total damage in the cladding material (E110) ~ 26,826 vacancies/ ion.This damage extends to depths of more than 10 µm inside the cladding material (Figure 10). Figure 11 shows the same damage calculations but for a coated cladding with a 9 µm thin film of metallic chromium.In this case, calculations show that the fuel cladding material will remain intact as the energetic Mo will be stopped inside the Cr with a relatively shorter range, the displacement damage created will be less as well.The maximum anticipated recoil energy for molybdenum (Mo) produced during the fission of nuclear fuel is about 120 MeV.This high energetic particle is expected to induce a total damage in the cladding material (E110) ~26,826 vacancies/ion.This damage extends to depths of more than 10 µm inside the cladding material (Figure 10). Figure 11 shows the same damage calculations but for a coated cladding with a 9 µm thin film of metallic chromium.In this case, calculations show that the fuel cladding material will remain intact as the energetic Mo will be stopped inside the Cr with a relatively shorter range, the displacement damage created will be less as well.The maximum anticipated recoil energy for molybdenum (Mo) produced during the fission of nuclear fuel is about 120 MeV.This high energetic particle is expected to induce a total damage in the cladding material (E110) ~ 26,826 vacancies/ ion.This damage extends to depths of more than 10 µm inside the cladding material (Figure 10). Figure 11 shows the same damage calculations but for a coated cladding with a 9 µm thin film of metallic chromium.In this case, calculations show that the fuel cladding material will remain intact as the energetic Mo will be stopped inside the Cr with a relatively shorter range, the displacement damage created will be less as well.The maximum damage that could be caused by rhodium (Rh) in E110 is shown in Figure 12.This is estimated to be ~ 29,895 vacancies/ion.It could be seen that this number is higher, when compared by the previous calculations, for the damage caused by Mo with the same maximum recoil energy which is estimated to be 26,826 vacancies/ ion.This difference is justifiable, given the variations in atomic masses for the two FPs, the higher the mass, the more the displacement damage, created by the high energetic particle.Lighter energetic ions will induce lower displacements, however; it will travel longer inside the target until come to rest, and this means longer implantation depths.A thin film of 9 µm in thickness will be able to contain this energetic FP (Figure 13) and eliminate its damaging effect on the nuclear fuel cladding material.The maximum damage that could be caused by rhodium (Rh) in E110 is shown in Figure 12.This is estimated to be ~29,895 vacancies/ion.It could be seen that this number is higher, when compared by the previous calculations, for the damage caused by Mo with the same maximum recoil energy which is estimated to be 26,826 vacancies/ion.This difference is justifiable, given the variations in atomic masses for the two FPs, the higher the mass, the more the displacement damage, created by the high energetic particle.Lighter energetic ions will induce lower displacements, however; it will travel longer inside the target until come to rest, and this means longer implantation depths.A thin film of 9 µm in thickness will be able to contain this energetic FP (Figure 13) and eliminate its damaging effect on the nuclear fuel cladding material.The maximum damage that could be caused by rhodium (Rh) in E110 is shown in Figure 12.This is estimated to be ~ 29,895 vacancies/ion.It could be seen that this number is higher, when compared by the previous calculations, for the damage caused by Mo with the same maximum recoil energy which is estimated to be 26,826 vacancies/ ion.This difference is justifiable, given the variations in atomic masses for the two FPs, the higher the mass, the more the displacement damage, created by the high energetic particle.Lighter energetic ions will induce lower displacements, however; it will travel longer inside the target until come to rest, and this means longer implantation depths.A thin film of 9 µm in thickness will be able to contain this energetic FP (Figure 13) and eliminate its damaging effect on the nuclear fuel cladding material.The calculated maximum damage induced by 120 MeV palladium (Pd) in the E110 alloy and the corresponding protective chromium coating thickness required is illustrated in Figures 14 and 15.Again, the calculations show that a thin Cr film ~ 9 µm will be capable enough to protect the fuel cladding from the damage induced by highly energetic Pd recoil, and contains this damage accordingly.The calculated maximum damage induced by 120 MeV palladium (Pd) in the E110 alloy and the corresponding protective chromium coating thickness required is illustrated in Figures 14 and 15.Again, the calculations show that a thin Cr film ~9 µm will be capable enough to protect the fuel cladding from the damage induced by highly energetic Pd recoil, and contains this damage accordingly.The calculated maximum damage induced by 120 MeV palladium (Pd) in the E110 alloy and the corresponding protective chromium coating thickness required is illustrated in Figures 14 and 15.Again, the calculations show that a thin Cr film ~ 9 µm will be capable enough to protect the fuel cladding from the damage induced by highly energetic Pd recoil, and contains this damage accordingly.The calculated maximum damage induced by 120 MeV palladium (Pd) in the E110 alloy and the corresponding protective chromium coating thickness required is illustrated in Figures 14 and 15.Again, the calculations show that a thin Cr film ~ 9 µm will be capable enough to protect the fuel cladding from the damage induced by highly energetic Pd recoil, and contains this damage accordingly.Figures 16-19 show the calculated damage, induced by the volatile species Iodine and Cesium, with/and without the application of a Cr film.These species are of particular interest in terms of their harmful impact on the zirconium based cladding materials, especially iodine, as it considered as a corrosive agent and a main contributor in SCC phenomenon.Calculations show that a thin chromium film of about 8 µm will successively lead to the containment of the damage that would be arise in the fuel cladding inner wall as a result of the presence of these two important fission products (Figures 17 and 19).Thus, by applying this 8 µm thin film on the inner surface of fuel cladding, the implantation of fission recoils inside the cladding will be prevented, and the hardening of inner-walls will be limited.Eventually; this will hinder, to a large extent, the appearance of cracks during reactor operation.This will result in limiting the presence of pathways to volatile fission species to migrate for longer depths inside the cladding and cause further corrosion and inner-surface degradation.
Figures 16-19 show the calculated damage, induced by the volatile species Iodine and Cesium, with/and without the application of a Cr film.These species are of particular interest in terms of their harmful impact on the zirconium based cladding materials, especially iodine, as it considered as a corrosive agent and a main contributor in SCC phenomenon.Calculations show that a thin chromium film of about 8 µm will successively lead to the containment of the damage that would be arise in the fuel cladding inner wall as a result of the presence of these two important fission products (Figures 17 and 19).Thus, by applying this 8 µm thin film on the inner surface of fuel cladding, the implantation of fission recoils inside the cladding will be prevented, and the hardening of innerwalls will be limited.Eventually; this will hinder, to a large extent, the appearance of cracks during reactor operation.This will result in limiting the presence of pathways to volatile fission species to migrate for longer depths inside the cladding and cause further corrosion and inner-surface degradation.Figures 16-19 show the calculated damage, induced by the volatile species Iodine and Cesium, with/and without the application of a Cr film.These species are of particular interest in terms of their harmful impact on the zirconium based cladding materials, especially iodine, as it considered as a corrosive agent and a main contributor in SCC phenomenon.Calculations show that a thin chromium film of about 8 µm will successively lead to the containment of the damage that would be arise in the fuel cladding inner wall as a result of the presence of these two important fission products (Figures 17 and 19).Thus, by applying this 8 µm thin film on the inner surface of fuel cladding, the implantation of fission recoils inside the cladding will be prevented, and the hardening of innerwalls will be limited.Eventually; this will hinder, to a large extent, the appearance of cracks during reactor operation.This will result in limiting the presence of pathways to volatile fission species to migrate for longer depths inside the cladding and cause further corrosion and inner-surface degradation.An important observation from the above calculations is that, metallic chromium has an increased ability to stop (stopping power) the energetic fission products simulated in this study, as these particles have longer average paths inside the zirconium alloy compared by metallic chromium.A comparison is shown in Figure 20, while the 120 MeV energetic Mo can travel inside the zirconium-based alloy for a depth of over 10 µm, it can be stopped inside Cr within a depth less than 8 µm.This may indicate the ability of chromium to withstand irradiation of energetic fission fragments for extended periods when compared to zirconium-based alloys, as the affected depth is much less in the former.This observation could also be closely linked to the remarks made on SCC phenomenon, in the sense that it does not affect pure metals as it does with alloys.Therefore, the classic approach to SCC prevention is based on the application of pure metal thin film on the inner side of the cladding tube [15] (zirconium liner in BWR and graphite in CANDU).An important observation from the above calculations is that, metallic chromium has an increased ability to stop (stopping power) the energetic fission products simulated in this study, as these particles have longer average paths inside the zirconium alloy compared by metallic chromium.A comparison is shown in Figure 20, while the 120 MeV energetic Mo can travel inside the zirconium-based alloy for a depth of over 10 µm, it can be stopped inside Cr within a depth less than 8 µm.This may indicate the ability of chromium to withstand irradiation of energetic fission fragments for extended periods when compared to zirconium-based alloys, as the affected depth is much less in the former.This observation could also be closely linked to the remarks made on SCC phenomenon, in the sense that it does not affect pure metals as it does with alloys.Therefore, the classic approach to SCC prevention is based on the application of pure metal thin film on the inner side of the cladding tube [15] (zirconium liner in BWR and graphite in CANDU).An important observation from the above calculations is that, metallic chromium has an increased ability to stop (stopping power) the energetic fission products simulated in this study, as these particles have longer average paths inside the zirconium alloy compared by metallic chromium.A comparison is shown in Figure 20, while the 120 MeV energetic Mo can travel inside the zirconium-based alloy for a depth of over 10 µm, it can be stopped inside Cr within a depth less than 8 µm.This may indicate the ability of chromium to withstand irradiation of energetic fission fragments for extended periods when compared to zirconium-based alloys, as the affected depth is much less in the former.This observation could also be closely linked to the remarks made on SCC phenomenon, in the sense that it does not affect pure metals as it does with alloys.Therefore, the classic approach to SCC prevention is based on the application of pure metal thin film on the inner side of the cladding tube [15] (zirconium liner in BWR and graphite in CANDU).

Conclusions
The use of thin film coatings on the internal surface of nuclear fuel cladding was proposed within the context of ATF, to provide further enhancement against corrosion and secondary hydrogenation.The inner surface thin film is expected to provide protection for the cladding material, against the effects of fission fragments, produced during the fission process, overcoming the fuel, and migrating to fuel cladding internal surface.Protection against wide range of radiation induced phenomena, and cladding material degradation will be offered.TRIM calculations were performed to study the ranges for a selected group of FPs that are experimentally observed, and mostly known to be linked to cladding inner-side degradation phenomena.The ranges were calculated inside the zirconium based alloy E110, to identify the depth that will be affected by these FPs, and evaluate the damage.As conservative approach, the maximum anticipated recoil energies for the studied group of FPs were used in the calculations.The expected damage caused by these products was also calculated.Based on this, a minimum thin chromium film of about 9 µm in thickness is recommended.This film is expected to offer sufficient protection and contain the energetic recoils, migrating to the inner wall of fuel cladding and play major role in its degradation.Thereby, limiting the inner-surface degradation and providing further enhancement for the zirconium based fuel cladding during normal operation and accidental conditions.The calculations also showed that metallic chromium had more stopping power and less total induced displacement damage in comparison with the Zrbased alloy.It is worth mentioning that, the calculated minimum thickness of Cr is not expected to significantly affect the reactor reactivity and would probably results in less than a 1% decrease in fuel cycle length according to calculations made by Novak and Sevecek [21].On the other hand, applying an inner surface thin film will provide protection for the fuel cladding against the internal corrosion and SCC, supporting the ability to increase fuel burnup during reactor operation as well as contributing to improved spent fuel management and waste minimization.However, the effects of this energetic FPs on metallic chromium thin film microstructure need to be thoroughly investigated and taken into account.

Conclusions
The use of thin film coatings on the internal surface of nuclear fuel cladding was proposed within the context of ATF, to provide further enhancement against corrosion and secondary hydrogenation.The inner surface thin film is expected to provide protection for the cladding material, against the effects of fission fragments, produced during the fission process, overcoming the fuel, and migrating to fuel cladding internal surface.Protection against wide range of radiation induced phenomena, and cladding material degradation will be offered.TRIM calculations were performed to study the ranges for a selected group of FPs that are experimentally observed, and mostly known to be linked to cladding innerside degradation phenomena.The ranges were calculated inside the zirconium based alloy E110, to identify the depth that will be affected by these FPs, and evaluate the damage.As conservative approach, the maximum anticipated recoil energies for the studied group of FPs were used in the calculations.The expected damage caused by these products was also calculated.Based on this, a minimum thin chromium film of about 9 µm in thickness is recommended.This film is expected to offer sufficient protection and contain the energetic recoils, migrating to the inner wall of fuel cladding and play major role in its degradation.Thereby, limiting the inner-surface degradation and providing further enhancement for the zirconium based fuel cladding during normal operation and accidental conditions.The calculations also showed that metallic chromium had more stopping power and less total induced displacement damage in comparison with the Zr-based alloy.It is worth mentioning that, the calculated minimum thickness of Cr is not expected to significantly affect the reactor reactivity and would probably results in less than a 1% decrease in fuel cycle length according to calculations made by Novak and Sevecek [21].On the other hand, applying an inner surface thin film will provide protection for the fuel cladding against the internal corrosion and SCC, supporting the ability to increase fuel burnup during reactor operation as well as contributing to improved spent fuel management and waste minimization.However, the effects of this energetic FPs on metallic chromium thin film microstructure need to be thoroughly investigated and taken into account.

Figure 3 .
Figure 3. Ion ranges for: (a) Pd with energy 19 MeV; (b) Ru with energy 12 MeV; and (c) Rh with energy 45 MeV, in E110 Alloy.The maximum implantation depths for this FPs are: 5.5 µm for Pd, 2.66 µm for Ru, and 5.7 µm for Rh respectively.

Figure 3 .
Figure 3. Ion ranges for: (a) Pd with energy 19 MeV; (b) Ru with energy 12 MeV; and (c) Rh with energy 45 MeV, in E110 Alloy.The maximum implantation depths for this FPs are: 5.5 µm for Pd, 2.66 µm for Ru, and 5.7 µm for Rh respectively.

Figure 3 .
Figure 3. Ion ranges for: (a) Pd with energy 19 MeV; (b) Ru with energy 12 MeV; and (c) Rh with energy 45 MeV, in E110 Alloy.The maximum implantation depths for this FPs are: 5.5 µm for Pd, 2.66 µm for Ru, and 5.7 µm for Rh respectively.

Figure 7 .
Figure 7. Damage caused by 120 MeV Tc in E110 alloy, coated with 8 µm thin film of Cr.

Figure 7 .
Figure 7. Damage caused by 120 MeV Tc in E110 alloy, coated with 8 µm thin film of Cr.

Figure 9 .
Figure 9. Damage caused by 120 MeV Ru in E110 alloy, coated with 9 µm thin film of Cr.

Figure 9 .
Figure 9. Damage caused by 120 MeV Ru in E110 alloy, coated with 9 µm thin film of Cr.

Figure 11 .
Figure 11.Damage caused by 120 MeV Mo in E110 alloy, coated with 9 µm thin film of Cr.

Figure 11 .
Figure 11.Damage caused by 120 MeV Mo in E110 alloy, coated with 9 µm thin film of

Figure 13 .
Figure 13.Damage caused by 120 MeV Rh in E110 alloy, coated with 9 µm thin film of Cr.

Figure 15 .
Figure 15.Damage caused by 120 MeV Pd in E110 alloy, coated with 9 µm thin film of Cr.

Figure 13 .
Figure 13.Damage caused by 120 MeV Rh in E110 alloy, coated with 9 µm thin film of Cr.

Figure 13 .
Figure 13.Damage caused by 120 MeV Rh in E110 alloy, coated with 9 µm thin film of Cr.

Figure 15 .
Figure 15.Damage caused by 120 MeV Pd in E110 alloy, coated with 9 µm thin film of Cr.

Figure 15 .
Figure 15.Damage caused by 120 MeV Pd in E110 alloy, coated with 9 µm thin film of Cr.

Figure 15 .
Figure 15.Damage caused by 120 MeV Pd in E110 alloy, coated with 9 µm thin film of Cr.

Table 1 .
Average chemical composition of E110 Alloy.