Supplemental Material 1 2 3 4 The Sm:YAG primary fluorescence pressure scale 5 6 7 8 Dmytro M. Trots,1 Alexander Kurnosov,1 Tiziana Boffa Ballaran,1 Sergey Tkachev,2 Kirill Zhuravlev,2 Vitali Prakapenka,2 Marek Berkowski,3 and Daniel J. Frost1 9 10 1 11 12 13 Germany. 2 GeoSoilEnviroCARS, University of Chicago, 9700 South Cass Ave. 434A, Argonne, IL 60439, 14 15 Bayerisches Geoinstitut, Universität Bayreuth, Universitätsstraße 30, D-95447 Bayreuth, USA. 3 Institute of Physics, Polish Academy of Science, Al. Lotnikow 32/46, 02-668 Warsaw, Poland. 16 17 18 19 20 Corresponding author: D. M. Trots, Bayerisches Geoinstitut, Universität Bayreuth, Universitätsstraße 30, D-95447 Bayreuth, Germany. (d_trots@yahoo.com) 21 22 1 25 Pressure (GPa) 20 (a) (b) (c) (d) (e) (f) (g) (h) (i) (j) (k) (l) 15 10 5 0 618 620 622 624 626 Pressure (GPa) Wavelength (nm) 50 45 (a) 40 (b) 35 (c) 30 (d) (e) 25 (f) 20 (g) (h) 15 (i) 10 (j) (k) 5 (l) 0 618 620 622 624 626 628 630 632 634 Wavelength (nm) Supplementary figure S1. Comparison of Y1-Sm:YAG calibrations. Calibration of fluorescence wavelength of Y1 band of Sm:YAG vs. absolute pressure and its comparison with other pressure scale dependent calibrations: (a) – Bi et al., [1990]; (b) – Hess and Schiferl, [1992]; (c)– Liu and Vohra, [1993]; (d) – Yusa et al., [1994], polynomial; (e) Yusa et al., [1994], linear; (f) – Zhao et al., [1998]; (g)– Sanchez-Valle et al., [2002]; (h) – Goncharov et al., [2005]; (i) – Raju et al., [2011]; (j)– Wei et al., [2011]; (k) – fit to our data; (l) – our data. 2 25 Pressure (GPa) 20 15 (a) (b) (c) (d) (e) (f) (g) (h) (i) 10 5 0 616 618 620 622 624 Pressure (GPa) Wavelength (nm) 60 55 50 45 40 (a) 35 (b) 30 (c) 25 (d) (e) 20 (f) 15 (g) 10 (h) 5 (i) 0 616 618 620 622 624 626 628 630 632 634 Wavelength (nm) Supplementary figure S2. Comparison of Y2-Sm:YAG calibrations. Calibration of fluorescence wavelength of Y2 band of Sm:YAG vs. absolute pressure and its comparison with other pressure scale dependent calibrations: (a) – Hess and Schiferl, [1992]; (b) – Liu and Vohra, [1993]; (c) – Yusa et al., [1994], polynomial; (d) Yusa et al., [1994], linear; (e)– Zhao et al., [1998]; (f)– Goncharov et al., [2005]; (g)– Raju et al., [2011]; (h) – fit to our data; (i) – our data. 3 Supplementary figure S3. Large single crystals of Sm:YAG were grown using the Czochralski method at the Institute of Physics, Polish Academy of Science. The crystals were each cut lengthwise and ICP MS measurements were performed on the sliced phases in 41 points for each crystal: the upper and lower crystals contain 0.5–0.7 and 1.7–2.2 wt % of Sm2O3, respectively. SINGLE CRYSTAL FRAGMENTS CAN BE PROVIDED ON REQUEST. 24 4 25 Supplementary methods: high-temperature powder diffraction 26 Thermal expansion measurements were performed at the synchrotron facility HASYLAB/DESY 27 (Hamburg, Germany) with the powder diffractometer at beam-line B2 [Knapp et al., 2004a]. The sample 28 was ground in an agate mortar and sieved through a mesh. A quartz capillary 0.3 mm in diameter was 29 filled with powdered Sm:YAG and sealed. Subsequently, the capillary was mounted inside a STOE 30 furnace in Debye–Scherrer geometry, equipped with a Eurotherm temperature controller and a capillary 31 spinner. The furnace temperature was measured by a TYPE–N thermocouple and calibrated using the 32 thermal expansion of NaCl [Pathak and Vasavada, 1970]. In order to avoid the adsorption of the K edge 33 from Yttrium around 0.73 Å, a wavelength of 0.74925(1) Å was selected using a Si(111) double flat- 34 crystal monochromator from the direct white synchrotron beam. The x-ray wavelength was determined 35 from eight reflection positions of LaB6 reference material (NIST SRM 660a) measured with a 36 scintillation single counter detector, which has Ge(111) analyser crystal in its front. Eighty-eight 37 diffraction patterns were collected for Sm:YAG (5-7 minutes per pattern depending on the synchrotron 38 ring current with 1 minute for temperature stabilization) at different temperatures up to 1197 K with a 39 temperature step of approximatelly 10 K during heating cycles, using an image-plate detector [Knapp et 40 al., 2004b]. The image plate detector was calibrated using the diffraction pattern of LaB6 and the 41 wavelength was determined using the tandem scintillation counter/analyser crystal. An additional pattern 42 was taken at ambient temperature after the heating cycle. All diffraction patterns were analyzed using 43 the software WinPLOTR [Rodriguez–Carvajal, 1993]. 44 Supplementary note 1: thermal expansion 45 The temperature dependence of the volumes the Sm:YAG measured at the powder diffraction 46 beamline B2 (see supplementary methods) is summarized in supplementary table S1. The temperature 47 evolution of the volume was expressed as [Fei, 1995]: 48 T V (T ) VR exp (T ) dT T R (S1) 5 49 where VR is the volume at a chosen reference temperature TR and (T) is the thermal expansion 50 coefficient. We fitted equation (S1) to the experimental V vs. T data at fixed experimental values of VR 51 and TR (taken at ambient temperature) with a simple 2nd order polynomial, i.e.: 52 (T)=a0+a1T+a2T2 53 This approach was found to give a suitable description of the experimental data and 54 determination of the volumetric thermal expansion coefficient 0 at room pressure and room 55 temperature. The fitted values a0 = 8.41(50)*10-6 K–1, a1= 4.31(15)*10-8 K–2 and a2= –2.49(11)*10-11 K– 56 3 (S2) yield an estimate for the thermal expansion coefficient at ambient conditions of 0=19.0(7)*10-6 K–1. 57 6 58 Supplementary table S1. Unit-cell volumes of Sm:YAG at 88 temperaturesa. T (K) V (Å3) T (K) V (Å3) T (K) V (Å3) T (K) V (Å3) 298 1735.15 519.3356 1743.473 734.3692 1753.031 963.7077 1764.158 314.9491 1735.692 528.9673 1743.999 744.3724 1753.734 974.8285 1764.733 324.9886 1736.078 538.6059 1744.212 754.403 1754.066 986.0417 1765.15 334.9712 1736.386 548.2527 1744.626 764.4622 1754.481 997.3526 1765.746 344.9022 1736.785 557.909 1745.126 774.5515 1755.075 1008.767 1766.04 354.7865 1737.046 567.5757 1745.431 784.6724 1755.587 1020.292 1766.576 364.6288 1737.406 577.254 1746.076 794.8264 1756.024 1031.932 1767.107 374.4337 1737.74 586.9449 1746.332 805.0154 1756.452 1043.695 1767.669 384.2052 1738.24 596.6491 1747.016 815.2411 1756.929 1055.589 1768.161 393.9473 1738.561 606.3677 1747.395 825.5056 1757.515 1067.619 1768.657 403.6638 1738.856 616.1014 1747.509 835.8111 1758.053 1079.795 1769.272 413.3581 1739.295 625.851 1748.245 846.1598 1758.525 1086.055 1769.711 423.0335 1739.655 635.6173 1748.703 856.5543 1758.845 1097.09 1770.12 432.6932 1739.92 645.401 1749.052 866.9973 1759.466 1108.15 1770.45 442.3399 1740.407 655.2029 1749.453 877.4917 1759.974 1119.233 1771.236 451.9764 1740.872 665.0238 1749.933 888.0404 1760.504 1130.341 1771.755 461.6052 1741.098 674.8644 1750.412 898.6468 1761.069 1141.473 1772.353 471.2285 1741.576 684.7255 1750.783 909.3144 1761.687 1152.629 1772.626 480.8487 1741.933 694.608 1751.429 920.0468 1762.006 1163.81 1773.343 490.4677 1742.255 704.5127 1751.647 930.848 1762.58 1175.014 1773.929 500.0873 1742.663 714.4404 1752.332 941.7223 1763.102 1186.243 1774.426 509.7094 1743.29 724.3923 1752.817 952.6739 1763.422 1197.495 1775.069 59 a Standard deviations of volumes are of the order of 0.1 Å3 as obtained from a whole–profile fitting 60 procedure. 61 62 7 63 Supplementary note 2: EoS formalism and determination of absolute pressure 64 Physical properties at ambient conditions and estimation of the magnitude of the 65 adiabatic–to–isothermal correction 66 The room temperature volume V0 was measured precisely three times from three different pieces 67 of Sm:YAG by single crystal diffraction using the 8–positions centring procedure and refined using the 68 vector least square algorithm implemented in the code Single [Angel and Finger, 2011]. The values for 69 V0 displayed a maximum difference of only 0.03%. Therefore, we have set the mean value 70 V0=1735.15(0.26) Å3 for the ambient pressure volume. Using compositional constraints from laser 71 ablation ICP MS, the calculated density, 0, is equal to 4678.7(7) kg/m3. 72 The acoustic sound velocities of two different single crystal fragments of Sm:YAG were 73 measured by Brillouin spectroscopy at ambient conditions. The values for adiabatic bulk moduli for both 74 fragments were derived from the sound velocity data. They lie within the estimated standard deviations 75 (Table 1). The value for adiabatic bulk modulus KS0 at ambient conditions is, thus, set to the mean value 76 of 186.5(1.5) GPa as measured by Brillouin spectroscopy. By analogy, the room pressure Debye 77 temperature 0= 730(10) K was averaged from two determinations, which were calculated from 78 experimental sound velocities using the equation of Robie and Edwards [1966]: 79 1 1 1 h n 3 3 1 2 3 3 0 3 k 4V0 VP 0 3 VS 0 3 (S3) 80 where h is the Plank constant, k is the Boltzmann constant, n = 160 – the number of atoms in the unit 81 cell, and VP0 and VS0 are the experimental longitudinal and transverse velocities at ambient conditions, 82 respectively. The applicability of this equation is also supported by the fact that Konigs et al. [1998] 83 have shown that the dependency of the heat capacity vs. temperature obeys the Debye theory. 84 The value of the room pressure Grüneisen parameter 0 is determined via: 85 0 0KS 0 0C p 0 (S4) 8 86 and it is equal to 1.32(0.13), where Cp0 = 571.72 J*kg-1*K-1 is the experimental isobaric heat capacity of 87 yttrium aluminum garnet at room temperature determined by [Konigs et al., 1998]. 88 The isothermal bulk modulus is calculated via equation (7), so that the value for the isothermal 89 bulk modulus KT0 at ambient conditions is equal to 185.1(1.5) GPa. The difference between the adiabatic 90 and isothermal values of the bulk modulus is only 0.7 %, whereas, according to Sinogeikin and Bass 91 [2000], the experimental accuracy in the determination of the elastic moduli using Brillouin scattering in 92 symmetric platelet geometry is approximately 1 %. Moreover, the adiabatic to isothermal correction will 93 be even smaller at higher pressures, because the thermal expansivity and Grüneisen parameter decrease 94 with pressure. We, therefore, expect that the results from fits of EoS before and after the adiabatic to 95 isothermal correction will be essentially the same within the experimental accuracy. In the following we 96 will perform fits of EoS parameters using both approaches, i.e. ignoring and accounting for the adiabatic 97 to isothermal correction to show that the correction is negligible for Sm:YAG. 98 EoS formalism and determination of absolute pressure 99 The third–order Eulerian finite strain EoS was used for the analysis of the volume data and 100 “cold” variation of the elastic moduli upon compression [Stixrude and Lithgow–Bertelloni, 2005]. 101 Initially, the adiabatic to isothermal correction was neglected when fitting equations (4) and (5) to the 102 experimental KS vs. V and G vs. V dependencies: the parameters V0, KT0`, G0, G0` were fitted, whereas, 103 according to recommendations of Kono et al. [2010] and Bass et al. [1981], the value for KT0 was kept 104 fixed to the value determined from the Brillouin data. 105 In order to check whether the adiabatic to isothermal correction is negligible, we used equation 106 (4), where, according to the thermodynamically self–consistent approach [Stixrude and Lithgow– 107 Bertelloni, 2005], the volume dependence of the Grüneisen parameter for isotropic solid is represented 108 as: 109 1 1 2 f 1 6 0 12 0 36 02 18 0 q0 f 1 6 2 2 1 6 0 f 2 12 0 36 0 18 0 q0 f (S5) 9 110 with 0 determined from equation S4 and q0 being the logarithmic volume derivative of the effective 111 Debye temperature. The isochoric heat capacity was evaluated within the framework of the Debye 112 theory, with the volume dependence incorporated into the volume dependence of the Debye 113 temperature: 114 CV 9nN A k B T 3 / T x 4e x e x 0 1 2 (S6) dx 1 115 1 2 0 1 6 0 f 12 0 36 02 18 0 q0 f 2 2 116 where NA is the Avogadro number and 0 is the room pressure value for the Debye temperature 117 determined by equation (S3). The fits of the equations (4),(5) and (S5)–(S7) to the experimental KS vs. V 118 and G vs. V dependencies were performed with fixed values of KT0, 0 and 0 calculated via equations 119 (7), (S4) and (S3), respectively. The parameters V0, KT0`, G0, G0` were fitted. By analogy with Kono et al. 120 [2010], q0 was kept fixed during the fitting procedure and was varied manually in the range from 1 to 8. 121 As can be seen from Table A1 in Stixrude and Lithgow–Bertelloni [2005], this range is typical for 122 numerous oxide silicates and aluminates. Only tiny changes of the V0, KT0`, G0, G0` parameters, lying 123 within the uncertainties, were found using the different q0 values, thus demonstrating the insensitivity of 124 EoS parameters to changes in q0. The analysis of Table A1 of reference [Stixrude and Lithgow– 125 Bertelloni, 2005] shows that q0=1.4 is typical for a number of garnets, therefore q0 was fixed to this 126 value during the final fit. (S7) 127 The results of weighted fits are summarized in Table 2 and illustrated in Fig. 2 together with the 128 experimental plots of KS vs. V and G vs. V. The weights in the fitting procedure were assigned according 129 to the effective variance method [Orear, 1982]. The standard errors for the fitted parameters were 130 derived from the variance–covariance matrix of the parameters estimates, which was found by 131 multiplying a matrix of partial derivatives, Jacobian matrix, by the mean squared errors. The values of 132 the EoS parameters obtained accounting for and ignoring the adiabatic-to-isothermal correction are very 10 133 similar, lying, typically, within 1% of the standard errors (Table 2). The only exception is the difference 134 in the value obtained for V0, which falls into the 1.5% standard errors. Thin lines in Fig. 2 represent the 135 confidence intervals of any KS and G values predicted by the EoS at any point along the range of V. 136 These intervals were obtained from the standard errors for the parameter estimates using Student’s t- 137 Distribution at the 99% confidence level, i.e. the 99% probability of the confidence range to capture the 138 true values for KS and G parameters. 139 The absolute pressure was determined using equation (6). The difference in absolute pressure 140 between the two sets of EoS parameters obtained with and without the adiabatic to isothermal correction 141 is 0.6 %, or 0.36 GPa, at the highest pressure. 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