Abstract
Zircon samples without and with secondary chemical alteration from diverse sources were subjected to heat treatment at 1400 °C for 96 h. Resulting new phases and textures suggest that decomposition of zircon into component oxides occurred in all experiments to various degrees. The crucible material was found to have a strong influence on the extent of breakdown, especially in the case of altered starting materials. In this study the progressive stages of the breakdown of zircon grains are described. The factors that may govern the decomposition are discussed, including radiation damage, secondary alteration and external reaction conditions (sample container, atmosphere). Alumina crucibles should generally be avoided in dry annealing of zircon, to minimise uncontrolled breakdown into oxides.
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Introduction
Zircon, ZrSiO4, is a common accessory mineral found in a wide range of igneous and metamorphic rocks. It is the most important mineral for U/Th–Pb geochronology because (i) zircon is an extremely robust container for parent U and Th and daughter isotopes through geologic time and (ii) this mineral mostly excludes Pb at primary growth. For industrial purposes, zircon is a widely used refractory material for high-temperature applications such as furnace linings, barrier coatings, ceramic pigments etc. In addition, zircon is the primary source for zirconium and zirconia (ZrO2).
Natural zircon has generally a non-ideal structure and composition, and industrial zircon is often processed, perhaps purified, natural zircon (see e.g. Pavlik et al. 2001). Depending on age, thermal history and actinide concentration, natural zircon has a certain level of accumulated radiation damage. The expected high-temperature behaviour of radiation-damaged (but not fully amorphised) zircon is a gradual restoration of short and long-range order (e.g. McLaren et al. 1994; Colombo and Chrosch 1998; Colombo et al. 1999; Begg et al. 2000; Capitani et al. 2000; Zhang et al. 2000; Nasdala et al. 2001; Geisler 2002; Nasdala et al. 2004). In contrast, the structural reconstitution of fully metamict zircon upon dry heating involves an intermediate stage of ZrO2 formation between 800 and 1100 °C, prior to the formation of crystalline zircon at above ca. 1150 °C (Mitsuhashi et al. 1974; Ellsworth et al. 1994; Zhang et al. 2000; Nasdala et al. 2002).
Pure, undamaged zircon is predicted to be stable up to ca. 1676 °C (e.g. Butterman and Foster 1967), at which point it decomposes into oxides. However, it is far from uncommon to observe that zircon breaks down at temperatures well below the thermodynamically predicted decomposition temperature. There appears to be no well-defined temperature for the onset of decomposition. Peña and de Aza (1984) and Kaiser et al. (2008) compiled zircon decomposition temperatures from the literature, ranging from 1400 °C to 2000 °C, but cited reports of incongruent melting at higher temperatures as well.
High-temperature treatment of zircon is done for various reasons in radioactive dating methods as well. The zircon whole-grain evaporation method (Kober 1986, 1987) utilises the decomposition of zircon into oxides (ZrO2 + SiO2) at elevated temperatures, where Pb is removed from zircon through the volatilisation of the silica component. Zircon evaporation is carried out on grains wrapped in inert rhenium filaments under vacuum (at ca. 1400–1500 °C). The “chemical abrasion” technique (multi-step leaching and thermal ionisation mass spectroscopy of whole zircon grains, CA-TIMS; Mattinson 2005) involves thermal preconditioning, prior to multi-step partial dissolution analysis, in order to partially stabilise radiation-damaged domains for a better-controlled etching behaviour. For this, Mattinson (2005) suggested to do heat treatment in air in alumina crucibles, at 800–1100 °C for 48 h. Note, however, that most geochronology laboratories seem to use SiO2 crucibles instead of alumina.
This paper presents results of annealing experiments aimed to observe the progress of the breakdown of zircon. In our study the temperature for heat treatment was chosen at 1400 °C. This temperature is within the reported range of decomposition temperatures, high enough to anneal radiation damage (not studied here), yet significantly below the thermodynamically expected decomposition temperature of zircon. We attempt to evaluate factors influencing the decomposition behaviour of zircon, with special attention to chemical alteration of radiation-damaged domains. The role of thermal breakdown in age determination methods involving high-temperature treatment is discussed.
Materials and methods
Table 1 gives a summary of materials and experiments in this study. Three types of samples were included. First, we studied pure (undoped), synthetic zircon single crystals (1–2 mm), grown using the Li–Mo flux method (Hanchar et al. 2001). Second, fragments (0.5–2 mm) of well-characterised, inclusion-free zircon crystals were also studied, including the 1064 Ma old sample 91500 from Ontario, Canada (Wiedenbeck et al. 2004), and the late Precambrian–Cambrian gemstones M257, M127 (Nasdala et al. 2008), M146 and M144 (Nasdala et al. 2004) from Sri Lanka. In addition, zircon grains (sample 87165; Pérez-Soba et al. 2007) from a coarse-grained leucogranite of the Hercynian La Pedriza pluton, Spanish Central System batholith, were also studied. This zircon was heavily altered by secondary hydrothermal processes, and consequently it is chemically impure, significantly hydrated and has a large number of pores and mineral inclusions (Nasdala et al. 2009).
Small (0.5–1 mm) euhedral grains or chips of larger crystals were heated in either platinum or sintered Al2O3 crucibles. The crucibles were covered with a lid of the same material and placed in a larger alumina crucible to further reduce the exchange of gaseous species between crucible and furnace atmosphere. The samples were heated at 1400 °C in high-temperature furnaces for 96 h. The heating rate was typically ca. 50 °C/min (fast heat-up). The furnaces were equipped with type B thermocouples, temperature was regulated by the built-in controllers, the temperature accuracy was better than 50 °C. After 96 h the furnaces were switched off. Samples were removed only after the furnaces had cooled to room temperature. An attempt was made to check the effect of the rate of heat-up: a set of unaltered samples (Table 1) was subjected to annealing with a very flat ramp (1 °C/min) in a Pt crucible.
Following heat treatment, outer surfaces of the samples were imaged on uncut grains. Some grains were then embedded in araldite epoxy, ground to approximately half thickness and polished to reveal internal textures for scanning electron microscope (SEM) imaging. For transmission electron microscopy (TEM) analyses, electron transparent foils were prepared with the focused ion beam (FIB) technique (Wirth 2004).
Secondary electron (SE) and back-scattered electron (BSE) images of unprepared grains (i.e., no polishing and carbon coating) were taken in a LEO EVO 60 variable-pressure SEM, used in the low-vacuum mode. Epoxy-mounted samples were carbon coated and imaged using a JEOL JSM-6400 SEM. Sub-micrometer textures and compositions on FIB foils were studied with an FEI Tecnai G2 F20 X-Twin analytical TEM operated at 200 kV in selected area electron diffraction (SAED), high-resolution (HRTEM) and scanning TEM (STEM) modes. For phase identification TEM and Raman spectroscopy were used. Raman spectra were acquired with a Renishaw RM1000 system in the quasi-confocal mode. The instrument was equipped with a Leica DMLM optical microscope, edge filter-based laser line rejection, an optical grating (1200 grooves/mm), and a Si-based, Peltier-cooled CCD detector. The 632.8 nm emission of a He-Ne laser was used as the excitation source, and the elastic (Rayleigh) scattering was used for spectral calibration. The spectral resolution of the system was ca. 2.2 cm−1; the wavenumber accuracy was better than 1 cm−1. Modal composition and pore space estimates were obtained from BSE images using the ImageJ image processing and analysis program (available at http://rsbweb.nih.gov/ij/). The method is based on the assumption that the volume fractions of different phases or pore space are represented by the relative two-dimensional surface areas of greyscale shades measured on cross-sections.
Results
All samples display, though to largely varying degrees, evidence of reactions after the heat treatment, partly on outer surfaces and partly also internally. Zirconium oxide as a reaction product has been observed in all samples after heat treatment. The monoclinic polytype (baddeleyite) has been identified at room temperature using Raman spectroscopy (Fig. 1) and TEM (electron diffraction and chemical analysis). Zirconia shows pronounced polysynthetic twinning (Fig. 2b), suggesting a transformation from a higher-symmetry polymorph upon cooling. Tetragonal ZrO2 has not been observed.
Silica has been found in the amorphous state, suggested by a diffuse ring in the TEM SAED patterns. TEM chemical point analysis reveals that silica contains impurity elements (Mg, Ca, Al, P) in the percent range. SiO2 is positively identified only in sample 87165, in Pt-annealed grains and in internal zones of alumina-annealed grains where a zircon matrix is found after heat treatment (Fig. 2a, c). A thin layer of an unidentified transparent material, seen as coloured interference fringes on a reflected-light optical microscope image, is observed in some reaction pits (e.g. on M257). Raman spectra recorded from these thin layers lack characteristic bands of any known SiO2 polymorph, but show a very high luminescence background (and peaks from underlying zircon). The thickness of these layers is estimated from the interference colours (assuming refractive index n = 1.5) to be less than 0.5 µm.
No strong evidence for the presence of silica is found in most of the reaction pits on the surfaces or in zirconia aggregates of heat-treated synthetic and unaltered samples (Figs. 3 and 4). Significant amounts of silica are “missing” from reaction zones that were in close contact with alumina crucibles. However, no reaction phase could be identified with Raman spectroscopy on the inner surface of the alumina crucibles at the sites of contact with the grains.
Decomposition textures have been observed either confined to outer surfaces or scattered throughout the volume of the grain. Surface breakdown has occurred in synthetic ZrSiO4 and natural, unaltered zircon samples (syn, M127, M257, M144, M146 and 91500), while the hydrothermally altered La Pedriza zircon (sample 87165) exhibits oxide phases in the interior of the grains as well.
Synthetic ZrSiO4 and unaltered zircon grains show only minor breakdown after being heated slowly (i.e., at ca. 50 °C/min) in Pt crucibles. The synthetic ZrSiO4 sample displays a great number of very small (<2 µm) reaction pits, whereas the natural grains have very few, slightly larger (up to 10 µm), isolated reaction pits on the grain surfaces. Somewhat different textures have developed after slow heating (ca. 1 °C/min) of the unaltered samples in a Pt crucible. There is again only minor breakdown, and all of the annealed fragments show zirconia grains that lie near the grain surfaces. However, some of these zirconia crystals are found underneath a thin (<5 µm) layer of zircon, while the rest sit recessed into the surface (Fig. 5a–b; compare Fig. 3a–b). No perceptible difference between bulk zircon and the thin cover layer was detected on SEM images (BSE brightness, texture). No trace of silica is observed on polished cross-cuts (Fig. 5b).
Synthetic ZrSiO4 and unaltered zircon samples annealed in alumina crucibles (fast heat-up) decompose more extensively, as shown in Fig. 3a–c. A peculiar feature is that a zirconia aggregate crust develops only on one side of the grain, namely on the side of the fragment, or face of the crystal, that was in physical contact with the crucible during annealing. After heating for 96 h, the reaction front (zircon–porous zirconia interface) has advanced 10–30 µm inwards from the original surface (Figs. 3c and 4). Note that on the same grains the faces that have not been in contact with alumina are sparsely covered with reaction pits and isolated zirconia grains.
From the observed abundance and extent of the breakdown that develops on outer surfaces (synthetic ZrSiO4 and unaltered samples), the progressive stages of the process may be reconstructed. The decomposition of synthetic ZrSiO4 and unaltered zircon during annealing usually starts at the outer surface and proceeds inwards (Figs. 3 and 4). The process starts with isolated, shallow pits on the surface, with a flat zirconia grain in the centre (Fig. 3a). As the decomposition proceeds, the pits grow laterally but not significantly in depth (Fig. 3b). The pits eventually merge and cover the entire surface, but the zirconia grains remain isolated. The further breakdown of zircon then advances away from the surface, and the zirconia grains are eventually sintered into a porous aggregate (Fig. 3c) when a zircon substrate supports them no longer. At this stage the reaction front proceeds inwards, roughly parallel to the surface, leaving a sponge-like zirconia network with very little or no silica. The breakdown may advance so far that the entire zircon material is consumed. The leftover zirconia aggregate retains the outer shape of the original zircon grain.
In annealed grains of sample 87165, the breakdown products are not limited to the surfaces. The zircon grains annealed (fast heat-up) in an alumina crucible show the most extensive breakdown: 80–100 vol% of each grain consists of a sponge-like, porous network of monoclinic zirconia (Fig. 2a–b) without observable traces of silica. The volume ratio of zirconia to pore space is estimated to be close to 50:50, with ±5% error. In some, but not all, grains there are areas of irregular shape where zircon is observed after heat treatment (Fig. 2a). Electron diffraction patterns made on FIB foils cut from such zircon zones reveal polycrystalline zircon. The crystallites are not oriented, suggesting recrystallisation without major directional control by epitaxial growth. There are tiny (0.1–2 µm), round inclusions, scattered irregularly in the zircon matrix. The inclusions are filled with amorphous silica that covers the walls and hosts a rounded ZrO2 grain. The centre of the inclusions is pore space (Fig. 2c).
Grains of sample 87165 annealed in a Pt crucible (fast heat-up) show a different internal texture. The formation of polycrystalline zircon is much more pronounced and coexisting silica glass and zirconia are also observed after the heat treatment (Fig. 2d). Zircon was identified in ca. 75–90% of the grain volume; the rest of the grains is made up of amorphous silica (8–17%), monoclinic zirconia (2–4%) and pore space (2–5%; Fig. 2d). (Note that these numbers are rough estimates, as the method used to derive them is strongly influenced by the resolution, the contrast and the noise of BSE images. Values for zirconia, silica and pore space may especially have large errors either due to small grain size or small differences in their greyscale levels.) Rounded silica–zirconia–pore inclusions (identical to those found in samples annealed in an alumina crucible, cf. Fig. 2c) are abundant.
Discussion
In the phase diagram of the ZrO2–SiO2 system published by Butterman and Foster (1967), pure ZrSiO4 was predicted to be stable up to 1676 ± 7 °C. Kamaev et al. (2005) refined the same stability limit at 1674 ± 7 °C. O’Neill (2006) predicted 1665 °C based on thermodynamical calculations. Most recently, Kaiser et al. (2008) arrived at the value of 1673 ± 10 °C. However, zircon decomposition at the above temperatures seems to be the exception rather than the rule. In this study, decomposition was observed at 1400 °C, Kober (1986) observed breakdown between 1380 and 1480 °C, Mursic et al. (1992) reported a temperature of 1477 °C, Pavlik et al. (2001) recorded 1285 °C, Wang et al. (2006) and Wanthanachaisaeng et al. (2006) saw reaction products after heat treatment at 1400 °C, while Davis (2007) inferred a phase separation below 1550 °C. (See also Peña and de Aza 1984 and Kaiser et al. 2008 for a list of other temperature data.) The appearance of zirconia was observed even at unusually low temperatures by Zhang et al. (2000: 852 °C) Capitani et al. (2000: 927 °C) and Nasdala et al. (2002: between 800 and 950 °C) in fully metamict starting materials.
Effects of radiation damage
The synthetic and unaltered samples used in this study span an initial range in radiation damage from zero (syn) to moderate (M146; see Table 1). The character and the extent of breakdown observed on these samples suggest that initial radiation damage up to moderate levels has little influence on thermal decomposition. This is in agreement with Chapman and Roddick (1994), who found that appreciably different U concentrations and self-irradiation levels (10 ppm U, 1334 Ma vs. 160 ppm U, 2680 Ma; very low to moderate radiation damage) had little or no effect on the rate of zircon decomposition in vacuum.
Moderate radiation damage means that amorphous damage clusters are isolated in a defect-rich crystalline matrix. At high temperatures, a “self-epitaxial” recrystallisation of the damaged volumes, besides point defect annealing, is expected to occur (see Ewing et al. 2003). In contrast, in completely metamict zircon essentially the entire volume is amorphous. Monaghan et al. (2005) stated that amorphous SiO2–ZrO2 mixtures are thermodynamically unstable with respect to a mixture of solid oxides. Calculations by Kim and McIntyre (2002) also show that amorphous ZrO2–SiO2 mixtures with composition between 40–90 mol% SiO2 should decompose into amorphous silica-rich and zirconia-rich phases at temperatures as low as 600 °C. Lucovsky and Rayner (2000) observed demixing of vapour-deposited Zr silicate films between 800 and 900 °C. Carrez et al. (2003) arrived at similar conclusions, i.e. at low temperatures amorphous ZrSiO4 should undergo spinoidal decomposition as the component oxides are in the immiscibility domain.
Thus, spontaneous disintegration into a mixture of oxides in the amorphous volume is expected to occur prior to recrystallisation of fully metamict zircon upon heating. The appearance of zirconia in heavily damaged primary (unaltered) zircon at very low temperatures (Zhang et al. 2000; Capitani et al. 2000 and Nasdala et al. 2002; see above) is therefore not due to a decomposition reaction but results from the demixing of amorphous (metamict) zircon into more stable oxides.
Effects of alteration
The chemical resistance of heavily damaged zircon is significantly decreased against dissolution (e.g. Lumpkin 2001). A reaction of damaged zircon with fluids often yields secondary zircon in which the original texture, major and minor element composition and isotope concentrations are modified (e.g. Geisler et al. 2002; Geisler et al. 2003a). Secondary, altered zircon, such as sample 87165, is generally porous with micrometre to nanometre-scale pores (Putnis 2002; Nasdala et al. 2009), enriched in non-formula elements (especially, P, Fe, Ca, Al etc.; e.g. Geisler et al. 2003b), mineral inclusions (e.g. xenotime) and hydrous species (Nasdala et al. 2009).
The high-temperature behaviour of strongly altered zircon (sample 87165) is poorly understood but alteration apparently has a profound influence on decomposition (Fig. 2). The effects of porosity, non-formula elements, mineral inclusions and hydrous content (Nasdala et al. 2009) are impossible to separate from each other. Enhanced porosity offers abundant pathways for element mobility in contrast to dense zircon. The “colourful” chemistry (non-formula elements in the percent range) is inferred to play a role in lowering temperatures of dissociation reactions and, along with solid (mineral) inclusions, has a strong influence on phase equilibria (see e.g. Peña and de Aza 1984). The hydrous species, apart from lowering reaction temperatures, may react with silica and may chemically bind to or volatilise available SiO2. In general, SiO2 appears to be significantly more mobile in altered than in unaltered zircon, as seen from the nearly complete reaction of silica with the alumina crucible (Fig. 2a). At the same time, the reassociation of silica with zirconia is apparently limited, suggested by the coexistence of the two phases after four days of annealing (Fig. 2c–d). Experimental results presented in this paper do not allow us to draw precise conclusions about the effect of alteration on the thermal behaviour of zircon.
Effect of reaction conditions
The decomposition in synthetic ZrSiO4 and unaltered samples is always related to outer surfaces, implying that the reaction is initiated by external influences, i.e. effects not related to bulk zircon properties. However, we have no direct explanation as to what actually starts the point corrosion, which then extends first into pits and then a breakdown front proceeding inwards.
The differences in the extent of breakdown between Pt and Al2O3 crucibles are attributed to the crucible material. Generally, surface corrosion (synthetic and unaltered samples) is more advanced in alumina-annealed grains (Figs. 2a, 3c and 4) compared to Pt-annealed analogues. The effect of alumina is most pronounced on the grain surfaces that were in physical contact with the alumina crucible: in these areas the breakdown reaction reached a clearly more advanced stage (Figs. 3c and 4). The same is observed on grains of sample 87165 (altered zircon), where free silica is seen after annealing in a Pt crucible, whereas very extensive silica removal is observed in alumina crucibles.
We assume that the silica reacted with alumina and the equilibrium shifted in favour of further decomposition. According to Zhao et al. (2003), a reaction between amorphous silica (a liquid state was suggested by Peña and de Aza 1984) and Al2O3, forming an aluminosilicate glass, occurs already below 1350 °C. However, without crystalline mullite seeds, mullite nucleates from an amorphous state only above 1400 °C (Zhao et al. 2003), which may well explain why no third phase was identified using Raman spectroscopy in alumina crucibles.
Similar conclusions can be drawn for the zircon inclusions in heat-treated ruby (Wang et al. 2006; Wanthanachaisaeng et al. 2006). In a zircon inclusion decomposition should not be observed if the host mineral is inert with respect to the breakdown products. This is not the case with corundum, and thus ZrO2 is formed because the reaction between SiO2 and Al2O3 forms an aluminosilicate phase, preventing the recrystallisation of zircon.
Our results seem to indicate that zircon is chemically less resistant than it is often assumed. Direct contact of zircon with a potentially reactive material should therefore be avoided during the high-temperature treatment of zircon gems. Also, for long-term nuclear waste storage purposes care should be taken to avoid contact between zircon as waste form and any container material that may react with silica.
A comparison of our results to other studies in the literature reveals that the reaction atmosphere also has an influence on the breakdown of zircon into component oxides well below the thermodynamic decomposition temperature. The products of the breakdown reaction (especially ZrO2) have been observed when annealing in air (e.g. under atmospheric pressure in this study), under vacuum (e.g. Kober 1986; 1987; Ansdell and Kyser 1993; Chapman and Roddick 1994), in a hot combustion atmosphere (Fritsch et al. 2006) and in a reducing, gaseous atmosphere (Gardner and Buchanan 1975; Barreiro et al. 2009) as well.
The reaction atmosphere appears to influence the activity of silica in the vicinity of the grain surfaces. We assume that the flow of volatile species away from the grain surface, following the concentration/pressure gradient, is the main driving force under vacuum. In a hot combustion atmosphere (significant H2O partial pressure), such as that found in gas turbine engines, Fritsch et al. (2006) suggested the reaction of SiO2 with water vapour forming volatile Si(OH)4. In a reducing atmosphere, Gardner and Buchanan (1975) suggested a direct volatilisation of SiO2 and its reduction into SiO by H2 or CO. In low-pressure experiments (10−3 atm) done in a graphite furnace, Barreiro et al. (2009) reported that an increasing partial pressure of O2 (2 × 10−9–2 × 10−4 atm) in the furnace resulted in an increase in the weight loss of heated zircon samples. They explained this trend by suggesting a reaction between the graphite furnace and oxygen to form CO, which then reduces SiO2 into volatile SiO. Pavlik et al. (2001) used mass spectroscopy to identify volatile SiO during vacuum heating of zircon, i.e. without a reducing atmosphere.
The zircon samples heated in reducing (Gardner and Buchanan 1975; Barreiro et al. 2009) and hot combustion atmospheres (Fritsch et al. 2006) develop porous zirconia crusts analogous to zircon heated in air (Figs. 3c and 4) or in vacuum (Ansdell and Kyser 1993; Chapman and Roddick 1994). We find it questionable that reducing agents (CO, H2) or water vapour actually reach the zircon–baddeleyite reaction front once it is covered by a porous zirconia crust. We instead think that a volatilisation of SiO2 occurs at or near the reaction front, SiO2(g) diffuses through porous zirconia into the furnace atmosphere and reduction (to SiO) or hydroxide formation (Si(OH)4) may occur only there, accelerating the reaction by decreasing the amount (partial pressure) of SiO2 available. The decomposition of zircon therefore is not caused, only indirectly enhanced, by reductive gases or water vapour. Gas flow, as in the experiments of Fritsch et al. (2006), further increases the removal of volatile species.
Air is essentially free of reducing gases (given that no reduction occurs in the heated furnace) and the concentration of water vapour is typically very low (<22.9 g m−3 at 25 °C, which becomes <4.1 g m−3 when heated to 1400 °C). We expect that if no reaction occurs between evaporated silica and the reaction atmosphere (N2, O2, CO2) and crucible material (e.g. Pt), the reaction rate will be lower in dry-air annealing compared to heat treatment in reductive or hydrous atmospheres. Furthermore, air pressure may also decrease the rate at which SiO2(g) diffuses away from the reaction environment, therefore we expect the advance of the zircon–baddeleyite reaction front to be slower in a non-reducing gas atmosphere than in vacuum.
Implications for age determination techniques
We propose that thermal decomposition of zircon plays a key role in the success of age determination techniques that employ heat treatment. Two techniques are briefly outlined and the role of thermal decomposition is explained below.
In the whole-grain zircon evaporation technique of Kober (1986, 1987) and related methods (Davis 2007) a zircon grain is wrapped in a strip of rhenium foil (evaporation filament) so that only a thin slit is open facing a second Re filament (ionisation filament). Heating the zircon grain up to ca. 1230 °C is found to remove lead loosely bound (adsorbed) on surfaces and from highly leached (altered) domains. After such preconditioning, successively higher-temperature evaporation steps between 1330–1530 °C are used to decompose and evaporate zircon domains with decreasing Pb loss (for more details see Kober 1987 and Ansdell and Kyser 1993). In the CA–TIMS technique (Mattinson 2005), thermal preconditioning of whole zircon grains is done at 800–1100 °C in air for 48 h. After heat treatment the U/Th–Pb system is analysed through stepwise dissolution and mass spectroscopy (partial dissolution analysis, PDA). The key to the success of PDA is the heat treatment; without annealing PDA is not so effective.
A common feature in the two techniques is that there is an evolution of the isotope ratios in progressive evaporation/dissolution steps from open-system (“discordant”) towards closed-system (“concordant”) character. Note that Kober (1986; 1987) and Ansdell and Kyser (1993) associated the later stages (i.e., higher temperatures) of breakdown with increasing crystallinity. The results in this study (compare Figs. 3c and 4) and those of Chapman and Roddick (1994) suggest that structural damage up to moderate levels is not a major factor that governs the decomposition reaction. We need to emphasize that structural damage due to self-irradiation does not directly induce Pb loss (or a change in composition in general), only diminishes the resistance of primary zircon against dissolution (leaching).
Our results suggest that in zircon evaporation experiments the decomposition temperature of different domains is a function of the extent of chemical alteration. This is reflected in the order in which the zircon domains undergo breakdown: Pb will be released successively from domains less and less affected by Pb leaching and/or enrichment. The last domains to decompose will have a closed isotope system (no alteration), seen as a plateau 207Pb/206Pb age in TIMS.
We propose that in a CA–TIMS experiment different processes occur in zircon domains according to their alteration levels. Moderately damaged but unaltered domains experience a recovery of crystallinity. In altered or amorphous zones a phase separation into component oxides takes place. Partially decomposed zircon or a mixture of oxides is expected to be less stable, while the resistance of recrystallised zircon domains is increased against dissolution by HF. Subsequent PDA steps are therefore able to separate zircon zones according to the extent of breakdown developed during thermal preconditioning. Alumina crucibles (Mattinson 2005) may have the effect of reacting with silica, enhancing the decomposition of zircon. Note that the onset temperature of aluminosilicate glass formation in the reaction between zircon and alumina was put to ca. 1100 °C by Zhao et al. (2003), which is just at the upper limit of zircon annealing in the CA–TIMS technique. Annealing of zircon in SiO2 crucibles, in contrast, may actually decrease the extent of breakdown by increasing silica activity in the reaction atmosphere. It appears worthwhile to test the two crucible materials against each other in a chemical abrasion experiment.
Conclusions
The high-temperature breakdown of unaltered zircon below the generally accepted thermodynamical dissociation temperature (1665–1676 °C) is a surface corrosion process producing crystalline ZrO2 and amorphous SiO2. Silica is inferred to evaporate below 1400 °C. The extent of the breakdown is controlled by temperature and processes that decrease SiO2 activity in the reaction environment, such as molecular flow or diffusion due to a concentration gradient, reaction of silica vapour with the atmosphere (e.g. reduction by H2, CO or hydroxide formation with water vapour), solid-state reactions (e.g. with the crucible or the furnace material) or transport by a gas stream in the experimental chamber. Therefore if minimum decomposition is desired, a small-volume inert (e.g. Pt) crucible and a non-reactive atmosphere (such as N2 or air) should be used to anneal zircon at high temperatures. Similar constraints may apply to containers designed to be used for nuclear waste storage.
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Acknowledgements
Samples studied in this research were kindly provided by J.M. Hanchar (synthetic zircon), M. Wiedenbeck (91500), W. Hofmeister (M127, M144, M146, M257), and C. Pérez-Soba (87165). Thanks are due to A. Wagner for the excellent sample preparation, and to B. Ullrich for obtaining a BSE image of an annealed La Pedriza zircon. We are grateful to I. Dódony and D.W. Davis for helpful discussions and suggestions. The constructive reviews by J.M. Hanchar and an anonymous expert, and detailed comments by associate editor A. Möller, greatly contributed to the manuscript. Partial funding for this study was provided by the European Commission through contract no. MEXC-CT-2005-024878 and by the Austrian Science Fund (FWF) through grant no. P20028-N10.
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Váczi, T., Nasdala, L., Wirth, R. et al. On the breakdown of zircon upon “dry” thermal annealing. Miner Petrol 97, 129–138 (2009). https://doi.org/10.1007/s00710-009-0087-9
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DOI: https://doi.org/10.1007/s00710-009-0087-9