The Thermodynamic Properties of the f-Elements and their Compounds. Part 2. The Lanthanide and Actinide Oxides Rudy J. M. Konings, Ondrej Beneš, Attila Kovács, Dario Manara, David Sedmidubský, Lev Gorokhov, Vladimir S. Iorish, Vladimir Yungman, E. Shenyavskaya, and E. Osina
Citation: Journal of Physical and Chemical Reference Data 43, 013101 (2014); doi: 10.1063/1.4825256 View online: http://dx.doi.org/10.1063/1.4825256 View Table of Contents: http://scitation.aip.org/content/aip/journal/jpcrd/43/1?ver=pdfcov Published by the AIP Publishing
This article is copyrighted as indicated in the article. Reuse of AIP content is subject to the terms at: http://scitation.aip.org/termsconditions. Downloaded to IP: 78.131.95.159 On: Sun, 27 Apr 2014 17:09:58 The Thermodynamic Properties of the f-Elements and their Compounds. Part 2. The Lanthanide and Actinide Oxides
Rudy J. M. Konings, a) Ondrej Beneš, Attila Kovács, Dario Manara, and David Sedmidubský b) European Commission, Joint Research Centre, Institute for Transuranium Elements, P.O. Box 2340, 76125 Karlsruhe, Germany
Lev Gorokhov, Vladimir S. Iorish, c) Vladimir Yungman, E. Shenyavskaya, and E. Osina Joint Institute for High Temperatures, Russian Academy of Sciences, 13-2 Izhorskaya Street, Moscow 125412, Russia
(Received 24 August 2012; accepted 4 March 2013; published online 10 January 2014)
A comprehensive review of the thermodynamic properties of the oxide compounds of the lanthanide and actinide elements is presented. The available literature data for the solid, liquid, and gaseous state have been analysed and recommended values are presented. In case experimental data are missing, estimates have been made based on the trends in the two series, which are extensively discussed. Ó 2014 Euratom. [http://dx.doi.org/10.1063/ 1.4825256]
CONTENTS 3.6.1. Polymorphism and melting point. . . . 15 3.6.2. Heat capacity and entropy ...... 15 3.6.3. Enthalpy of formation ...... 15 1. Introduction ...... 6 3.7. Nd2O3(cr,l)...... 16 2. Approach ...... 6 3.7.1. Polymorphism and melting point. . . . 16 2.1. Thermal functions of condensed phases . . . 6 3.7.2. Heat capacity and entropy ...... 16 2.2. Enthalpies of formation of condensed phases 7 3.7.3. Enthalpy of formation ...... 17 2.3. Thermal functions of gases ...... 7 3.8. Pm2O3(cr,l) ...... 17 2.4. Enthalpies of formation of gases ...... 8 3.8.1. Polymorphism and melting point. . . . 17 2.5. Consistency and completeness ...... 9 3.8.2. Heat capacity and entropy ...... 17 3. The Lanthanide Oxides in Solid and Liquid State 9 3.8.3. Enthalpy of formation ...... 18 3.1. La O (cr,l) ...... 9 2 3 3.9. Sm2O3(cr,l) ...... 18 3.1.1. Polymorphism and melting point. . . . 9 3.9.1. Polymorphism and melting point. . . . 18 3.1.2. Heat capacity and entropy ...... 9 3.9.2. Heat capacity and entropy ...... 18 3.1.3. Enthalpy of formation ...... 10 3.9.3. Enthalpy of formation ...... 19 3.2. CeO (cr,l)...... 11 2 3.10. Eu2O3(cr,l)...... 20 3.2.1. Melting point...... 11 3.10.1. Polymorphism and melting point. . . 20 3.2.2. Heat capacity and entropy ...... 11 3.10.2. Heat capacity and entropy ...... 20 3.2.3. Enthalpy of formation ...... 11 3.10.3. Enthalpy of formation ...... 21 3.3. Ce O (cr,l) ...... 12 2 3 3.11. Eu3O4(cr)...... 22 3.3.1. Polymorphism and melting point. . . . 12 3.11.1. Polymorphism and melting point. . . 22 3.3.2. Heat capacity and entropy ...... 12 3.11.2. Heat capacity and entropy ...... 22 3.3.3. Enthalpy of formation ...... 13 3.11.3. Enthalpy of formation ...... 22 3.4. PrO2(cr,l) ...... 13 3.12. EuO(cr)...... 22 3.4.1. Structure ...... 13 3.12.1. Polymorphism and melting point. . . 22 3.4.2. Heat capacity and entropy ...... 13 3.12.2. Heat capacity and entropy ...... 22 3.4.3. Enthalpy of formation ...... 14 3.12.3. Enthalpy of formation ...... 22 3.5. PrO (cr,l) ...... 14 1.833 3.13. Gd2O3(cr,l) ...... 23 3.5.1. Melting point...... 14 3.13.1. Polymorphism and melting point. . . 23 3.5.2. Heat capacity and entropy ...... 14 3.13.2. Heat capacity and entropy ...... 23 3.5.3. Enthalpy of formation ...... 14 3.13.3. Enthalpy of formation ...... 24 3.6. Pr O (cr,l) ...... 15 2 3 3.14. TbO2(cr)...... 24 3.14.1. Structure ...... 24 a)Electronic mail: [email protected]. 3.14.2. Heat capacity and entropy ...... 24 b)Permanent address: Institute of Chemical Technology, Technická 5, 16626 3.14.3. Enthalpy of formation ...... 24 Praha 6, Czech Republic. c) 3.15. Tb6O11(cr),Tb11O20(cr),Tb4O7(cr), Deceased on May 2012. Tb O (cr)...... 25 Ó 2014 Euratom. 7 12
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3.15.1. Structure ...... 25 4.9.2. Enthalpy of formation ...... 44 3.15.2. Heat capacity and entropy ...... 25 4.10. TbO(g) ...... 44 3.15.3. Enthalpy of formation ...... 25 4.10.1. Heat capacity and entropy ...... 44 3.16. Tb2O3(cr,l)...... 25 4.10.2. Enthalpy of formation ...... 45 3.16.1. Polymorphism and melting point. . . 25 4.11. DyO(g) ...... 45 3.16.2. Heat capacity and entropy ...... 25 4.11.1. Heat capacity and entropy ...... 45 3.16.3. Enthalpy of formation ...... 26 4.11.2. Enthalpy of formation ...... 46 3.17. Dy2O3(cr,l) ...... 26 4.12. HoO(g) ...... 46 3.17.1. Polymorphism and melting point. . . 26 4.12.1. Heat capacity and entropy ...... 46 3.17.2. Heat capacity and entropy ...... 26 4.12.2. Enthalpy of formation ...... 47 3.17.3. Enthalpy of formation ...... 27 4.13. ErO(g)...... 48 3.18. Ho2O3(cr,l) ...... 27 4.13.1. Heat capacity and entropy ...... 48 3.18.1. Polymorphism and melting point. . . 27 4.13.2. Enthalpy of formation ...... 49 3.18.2. Heat capacity and entropy ...... 27 4.14. TmO(g)...... 49 3.18.3. Enthalpy of formation ...... 28 4.14.1. Heat capacity and entropy ...... 49 3.19. Er2O3(cr,l) ...... 29 4.14.2. Enthalpy of formation ...... 50 3.19.1. Polymorphism and melting point. . . 29 4.15. YbO(g) ...... 50 3.19.2. Heat capacity and entropy ...... 29 4.15.1. Heat capacity and entropy ...... 50 3.19.3. Enthalpy of formation ...... 29 4.15.2. Enthalpy of formation ...... 51 3.20. Tm2O3(cr,l) ...... 30 4.16. LuO(g) ...... 52 3.20.1. Polymorphism and melting point. . . 30 4.16.1. Heat capacity and entropy ...... 52 3.20.2. Heat capacity and entropy ...... 30 4.16.2. Enthalpy of formation ...... 52 3.20.3. Enthalpy of formation ...... 31 5. The Actinide Oxides in Solid 3.21. Yb2O3(cr,l) ...... 31 and Liquid State ...... 53 3.21.1. Polymorphism and melting point. . . 31 5.1. Ac2O3(cr,l)...... 53 3.21.2. Heat capacity and entropy ...... 31 5.1.1. Polymorphism and melting point. . . . 53 3.21.3. Enthalpy of formation ...... 31 5.1.2. Heat capacity and entropy ...... 53 3.22. Lu2O3(cr,l)...... 31 5.1.3. Enthalpy of formation ...... 53 3.22.1. Melting point ...... 31 5.2. ThO2(cr,l)...... 53 3.22.2. Heat capacity and entropy ...... 32 5.2.1. Melting point...... 53 3.22.3. Enthalpy of formation ...... 32 5.2.2. Heat capacity and entropy ...... 53 4. The Gaseous Lanthanide Oxides ...... 32 5.2.3. Enthalpy of formation ...... 54 4.1. LaO(g)...... 32 5.3. PaO2(cr,l)...... 54 4.1.1. Heat capacity and entropy ...... 32 5.3.1. Melting point...... 54 4.1.2. Enthalpy of formation ...... 33 5.3.2. Heat capacity and entropy ...... 54 4.2. CeO2(g)...... 34 5.3.3. Enthalpy of formation ...... 54 4.2.1. Heat capacity and entropy ...... 34 5.4. γ-UO3...... 54 4.2.2. Enthalpy of formation ...... 34 5.4.1. Polymorphism...... 54 4.3. CeO(g)...... 35 5.4.2. Heat capacity and entropy ...... 55 4.3.1. Heat capacity and entropy ...... 35 5.4.3. Enthalpy of formation ...... 55 4.3.2. Enthalpy of formation ...... 35 5.5. U3O8(cr) ...... 55 4.4. PrO(g) ...... 36 5.5.1. Polymorphism and melting point. . . . 55 4.4.1. Heat capacity and entropy ...... 36 5.5.2. Heat capacity and entropy ...... 55 4.4.2. Enthalpy of formation ...... 37 5.5.3. Enthalpy of formation ...... 56 4.5. NdO(g) ...... 37 5.6. U4O9(cr) ...... 56 4.5.1. Heat capacity and entropy ...... 37 5.6.1. Polymorphism...... 56 4.5.2. Enthalpy of formation ...... 39 5.6.2. Heat capacity and entropy ...... 56 4.6. PmO(g) ...... 39 5.6.3. Enthalpy of formation ...... 56 4.6.1. Heat capacity and entropy ...... 39 5.7. UO2(cr,l)...... 56 4.6.2. Enthalpy of formation ...... 40 5.7.1. Melting point...... 56 4.7. SmO(g) ...... 40 5.7.2. Heat capacity and entropy ...... 57 4.7.1. Heat capacity and entropy ...... 40 5.7.3. Enthalpy of formation ...... 58 4.7.2. Enthalpy of formation ...... 41 5.8. Np2O5(cr,l)...... 58 4.8. EuO(g)...... 42 5.8.1. Crystal structure ...... 58 4.8.1. Heat capacity and entropy ...... 42 5.8.2. Heat capacity and entropy ...... 58 4.8.2. Enthalpy of formation ...... 42 5.8.3. Enthalpy of formation ...... 58 4.9. GdO(g) ...... 43 5.9. NpO2(cr,l) ...... 58 4.9.1. Heat capacity and entropy ...... 43 5.9.1. Melting point...... 58
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5.9.2. Heat capacity and entropy ...... 58 6.9.2. Enthalpy of formation ...... 74 5.9.3. Enthalpy of formation ...... 59 6.10. NpO(g) ...... 75 5.10. PuO2(cr,l)...... 59 6.10.1. Heat capacity and entropy ...... 75 5.10.1. Melting point ...... 59 6.10.2. Enthalpy of formation ...... 75 5.10.2. Heat capacity and entropy ...... 59 6.11. PuO3(g)...... 75 5.10.3. Enthalpy of formation ...... 60 6.11.1. Heat capacity and entropy ...... 75 5.11. Pu2O3(cr,l)...... 60 6.11.2. Enthalpy of formation ...... 76 5.11.1. Polymorphism and melting point. . . 60 6.12. PuO2(g)...... 76 5.11.2. Heat capacity and entropy ...... 60 6.12.1. Heat capacity and entropy ...... 76 5.11.3. Enthalpy of formation ...... 61 6.12.2. Enthalpy of formation ...... 77 5.12. AmO2(cr,l)...... 61 6.13. PuO(g)...... 78 5.12.1. Melting point ...... 61 6.13.1. Heat capacity and entropy ...... 78 5.12.2. Heat capacity and entropy ...... 61 6.13.2. Enthalpy of formation ...... 79 5.12.3. Enthalpy of formation ...... 61 6.14. AmO2(g)...... 79 5.13. Am2O3(cr,l)...... 62 6.14.1. Heat capacity and entropy ...... 79 5.13.1. Polymorphism and melting point. . . 62 6.14.2. Enthalpy of formation ...... 79 5.13.2. Heat capacity and entropy ...... 62 6.15. AmO(g) ...... 79 5.13.3. Enthalpy of formation ...... 62 6.15.1. Heat capacity and entropy ...... 79 5.14. Cm2O3(cr) ...... 62 6.15.2. Enthalpy of formation ...... 80 5.14.1. Polymorphism and melting point. . . 62 6.16. CmO(g)...... 80 5.14.2. Heat capacity and entropy ...... 63 6.16.1. Heat capacity and entropy ...... 80 5.14.3. Enthalpy of formation ...... 63 6.16.2. Enthalpy of formation ...... 81 5.15. BkO2(cr) and Bk2O3(cr) ...... 63 6.17. Computed data for AnO(g) and AnO2(g) 5.15.1. Polymorphism and melting point. . . 63 (An ¼ Bk–Lr) ...... 81 5.15.2. Heat capacity and entropy ...... 63 7. Discussion and Conclusions...... 82 5.15.3. Enthalpy of formation ...... 63 7.1. Comparison to existing reviews ...... 82 5.16. CfO2(cr) and Cf2O3(cr)...... 63 7.2. Trends ...... 82 5.16.1. Polymorphism and melting point. . . 63 7.2.1. The crystalline sesquioxides ...... 82 5.16.2. Heat capacity and entropy ...... 64 7.2.2. The crystalline dioxides...... 84 5.16.3. Enthalpy of formation ...... 64 7.2.3. The gaseous monoxides...... 86 6. The Gaseous Actinide Oxides ...... 64 7.3. Recommendations for further research . . . . 87 6.1. AcO(g) ...... 64 Acknowledgments ...... 88 6.1.1. Heat capacity and entropy ...... 64 8. References ...... 88 6.1.2. Enthalpy of formation ...... 64 6.2. ThO2(g)...... 64 6.2.1. Heat capacity and entropy ...... 64 List of Tables 6.2.2. Enthalpy of formation ...... 65 6.3. ThO(g)...... 66 1. Nomenclature of the molecular properties for the 6.3.1. Heat capacity and entropy ...... 66 di- and polyatomic species ...... 8 6.3.2. Enthalpy of formation ...... 67 2. Temperature of melting of lanthanum sesquioxide 15 6.4. PaO2(g)...... 67 (after Coutures and Rand )...... 9 6.4.1. Heat capacity and entropy ...... 67 3. The enthalpy of formation of La2O3(cr) at 298.15 D D 6.4.2. Enthalpy of formation ...... 68 K; H1 is the enthalpy of solution of La(cr), H2 6.5. PaO(g) ...... 68 of La2O3(cr) in HCl(aq), respectively (after Cord- 6.5.1. Heat capacity and entropy ...... 68 funke and Konings34) ...... 10 6.5.2. Enthalpy of formation ...... 69 4. Temperature of melting of cerium dioxide . . . . . 11 6.6. UO3(g)...... 69 5. Temperature of melting of cerium sesquioxide 6.6.1. Heat capacity and entropy ...... 69 (after Coutures and Rand15)...... 12 6.6.2. Enthalpy of formation ...... 70 6. The enthalpy of formation of Ce2O3(cr) at 298.15 D D 6.7. UO2(g)...... 70 K; H1 and H2 are the enthalpies of solution of 6.7.1. Heat capacity and entropy ...... 70 Ce(cr) and Ce2O3(cr) in HCl(aq), respectively 6.7.2. Enthalpy of formation ...... 71 (after Cordfunke and Konings34) ...... 13 6.8. UO(g)...... 72 7. The enthalpy of formation of PrO1.833 and D D 6.8.1. Heat capacity and entropy ...... 72 Pr2O3(cr) at 298.15 K; H1 and H2 are the 6.8.2. Enthalpy of formation ...... 73 enthalpies of solution of Pr(cr) and PrO1.833(cr) 6.9. NpO2(g)...... 73 in HNO3(aq), Pr(cr) and Pr2O3(cr) in HCl(aq), 6.9.1. Heat capacity and entropy ...... 73 respectively (after Cordfunke and Konings34).. 14
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8. The enthalpy of formation of phases in the PrO2- 29. Molecular constants of LaO(g) ...... 33 1 PrO1.5 system ...... 15 30. The enthalpy of formation of LaO(g), in kJ mol 34 9. Temperature of melting of praseodymium 31. The molecular parameters for CeO2(g)...... 34 sesquioxide ...... 15 32. The enthalpy of formation of CeO2(g) at 298.15 K 35 10. Temperature of melting of neodymium sesqui- 33. Molecular constants of CeO(g) ...... 36 oxide (after Coutures and Rand15)...... 16 34. The enthalpy of formation of CeO(g), in kJ mol 1 36 141 16 11. The enthalpy of formation of Nd2O3(cr) at 298.15 35. Molecular constants of Pr O(g) ...... 37 D D 1 K; H1 and H2 are the enthalpies of solution of 36. The enthalpy of formation of PrO(g), in kJ mol 38 142 16 Nd(cr) and Nd2O3(cr) in HCl(aq), respectively 37. Molecular constants of Nd O(g)...... 38 (after Cordfunke and Konings34) ...... 17 38. The enthalpy of formation of NdO(g), in kJ mol 1 39 12. Temperature of melting of samarium sesquioxide 39. Molecular constants of 145Pm16O(g) ...... 40 (after Coutures and Rand15)...... 18 40. Molecular constants of 152Sm16O(g) ...... 41 1 13. The enthalpy of formation of Sm2O3(cr) at 298.15 41. The enthalpy of formation of SmO(g), in kJ mol 41 D D 153 16 K; H1 and H2 are the enthalpies of solution of 42. Molecular constants of Eu O(g)...... 42 1 Sm(cr) and Sm2O3(cr) in HCl(aq), respectively 43. The enthalpy of formation of EuO(g), in kJ mol 43 (after Cordfunke and Konings34) ...... 19 44. Molecular constants of 158Gd16O(g)...... 43 14. Temperature of melting of europium sesquioxide 45. The enthalpy of formation of GdO(g), in kJ mol 1 44 (after Coutures and Rand15)...... 20 46. Molecular constants of 159Tb16O(g)...... 45 15. The enthalpy of formation of monoclinic 47. Molecular constants of 159Dy16O(g)...... 46 D D 165 16 Eu2O3(cr) at 298.15 K; H1 and H2 are the 48. Molecular constants of Ho O(g)...... 47 1 enthalpies of solution of Eu(cr) and Eu2O3(cr) in 49. The enthalpy of formation of HoO(g), in kJ mol 48 HCl(aq), respectively ...... 21 50. Molecular constants of 166Er16O(g) ...... 48 16. Temperature of melting of gadolinium sesquiox- 51. The enthalpy of formation of ErO(g), in kJ mol 1 49 ide (after Coutures and Rand15) ...... 23 52. Molecular constants of 169Tm16O(g) ...... 49 1 17. The enthalpy of formation of Gd2O3(cr) at 298.15 53. The enthalpy of formation of TmO(g), in kJ mol 50 D D 174 16 K; H1 and H2 are the enthalpies of solution of 54. Molecular constants of Yb O(g)...... 51 1 Gd(cr) and Gd2O3(cr) in HCl(aq), respectively 55. The enthalpy of formation of YbO(g), in kJ mol 51 (after Cordfunke and Konings34) ...... 24 56. Molecular constants of 175Lu16O(g)...... 52 1 18. The enthalpy of formation of phases in the TbO2- 57. The enthalpy of formation of LuO(g), in kJ mol 52 TbO1.5 system ...... 25 58. Temperature of melting of thorium dioxide . . . . 53 19. Temperature of melting of terbium sesquioxide 59. Temperature of melting of uranium dioxide. . . . 57 15 (after Coutures and Rand )...... 25 60. The melting point of PuO2(cr)...... 59 20. The enthalpy of formation of Tb2O3(cr) at 298.15 61. The enthalpy of formation of plutonium dioxide 60 D D K; H1 and H2 are the enthalpies of solution of 62. Temperature of melting of plutonium sesquioxide 60 Tb(cr) and Tb2O3(cr) in HCl(aq), respectively 63. The melting point of Cm2O3(cr) ...... 62 (after Cordfunke and Konings34) ...... 26 64. Molecular constants of AcO(g) ...... 64 21. Temperature of melting of dysprosium sesqui- 65. The molecular parameters for ThO2(g)...... 65 15 oxide (after Coutures and Rand )...... 27 66. The enthalpy of sublimation of ThO2(g), in kJ 1 22. The enthalpy of formation of Dy2O3(cr) at 298.15 mol ...... 65 D D 67. Molecular constants of 232Th16O(g)...... 66 K; H1 and H2 are the enthalpies of solution of 1 Dy(cr) and Dy2O3(cr) in HCl(aq), respectively 68. The enthalpy of formation of ThO(g), in kJ mol 67 34 (after Cordfunke and Konings ) ...... 27 69. The molecular parameters for PaO2(g)...... 68 231 16 23. Temperature of melting of holmium sesquioxide 70. Molecular constants of Pa O(g) ...... 68 15 (after Coutures and Rand )...... 28 71. The molecular parameters for UO3(g)...... 69 1 24. The enthalpy of formation of Ho2O3(cr) at 298.15 72. The enthalpy of formation of UO3(g), in kJ mol 70 D D 73. The molecular parameters for UO (g)...... 71 K; H1 and H2 are the enthalpies of solution of 2 Ho(cr) and Ho2O3(cr) in HCl(aq), respectively 74. The enthalpy of sublimation of UO2(g), in kJ 1 (after Cordfunke and Konings34) ...... 28 mol ...... 72 238 16 25. Temperature of melting of erbium sesquioxide 75. Molecular constants of U O(g)...... 72 1 (after Coutures and Rand15)...... 29 76. The enthalpy of formation of UO(g), in kJ mol 73 26. The enthalpy of formation of Er2O3(cr) at 298.15 77. The molecular parameters for NpO2(g)...... 74 237 16 K; DH and DH are the enthalpies of solution of 78. Molecular constants of Np O(g)...... 75 1 2 1 Er(cr) and Er2O3(cr) in HCl(aq), respectively 79. The enthalpy of formation of NpO(g), in kJ mol 75 34 (after Cordfunke and Konings ) ...... 30 80. The molecular parameters for PuO3(g)...... 76 27. Temperature of melting of ytterbium sesquioxide 81. The molecular parameters for PuO2(g)...... 77 239 16 (after Coutures and Rand15)...... 31 82. Molecular constants of Pu O(g)...... 78 28. Temperature of melting of lutetium sesquioxide 83. The molecular parameters for AmO2(g)...... 79 243 16 (after Coutures and Rand15)...... 32 84. Molecular constants of Am O(g)...... 80
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90 85. Molecular constants of 247Cm16O(g) ...... 80 Pankratz et al. ; , value derived from the low- 86. Molecular constants and enthalpies of formation temperature measurements by Justice and Wes- 113 for AnO(g) (An ¼ Bk–Lr)...... 81 trum Jr. ; the curve shows the recommended 87. Molecular constants and enthalpies of formation equation...... 1 1 for AnO2(g)(An= Bk–Lr)...... 81 11. The reduced enthalpy increment (in J K mol ) 169 88. Selected thermodynamic data of the solid and of Er2O3; ○, Tsagareishvili and Gvelesiani ; &, liquid phases of the lanthanide and actinide oxides 83 Pankratz et al.90; , value derived from the low- 89. Selected thermodynamic data of the gaseous temperature measurements by Justice and Wes- lanthanide and actinide oxides...... 85 trum Jr.161; the curve shows the recommended equation...... 29 12. The reduced enthalpy increment (in J K 1 mol 1) 129 List of Figures of Tm2O3; ○, Tsagareishvili and Gvelesiani ; &, Pankratz et al.90; , value derived from the low- 1. The temperature corrections according to various temperature measurements by Justice et al.174; the temperature scales...... 7 curve shows the recommended equation...... 30 2. The reduced enthalpy increment (in J K 1 mol 1) 13. The reduced enthalpy increment (in J K 1 mol 1) 29 129 of La2O3; ○, Blomeke and Ziegler ; △, Yashvili of Yb2O3; ○, Tsagareishvili and Gvelesiani ; &, et al.30; ~, King et al.27; ^, Sedmidubský et al.31; Pankratz et al.90; , value derived from the low- , value derived from the low-temperature mea- temperature measurements by Justice et al.174; the surements by Justice and Westrum, Jr.;28 the curve curve shows the recommended equation...... 31 shows the recommended equation...... 9 14. The reduced enthalpy increment (in J K 1 mol 1) 1 1 30 3. The reduced enthalpy increment (in J K mol ) of Lu2O3; ○, Yashvili et al. ; &, Pankratz and 57 27 65 of CeO2; ○, Kuznetsov et al. ; &, King et al. ; Kelly ; , value derived from the low-tempera- ~, Mezaki et al.59; 5, Yashvili et al.60; ◊, Pears ture measurements by Justice et al.174; the curve et al.58; , value derived from the low-temperature shows the recommended equation...... 32 measurements by Westrum, Jr. and Beale, Jr.;56 the 15. The reduced enthalpy increment (in J K 1 mol 1) 317 curve shows the recommended equation...... 11 of ThO2; , Jaeger and Veenstra ; ~, South- 318 319 58 4. The polymorphism in the Ln2O3 series as a func- ard ; &, Hoch and Johnston ; * Pears et al. ; tion of temperature...... 12 ^, Victor and Douglas320; , Springer et al.321; 5. The enthalpy of formation of compositions in the 5, Fischer et al.323; (, Agarwal et al.324; Dash 325 314 PrO2-PrO1.5 (&) and TbO2-TbO1.5 (&) systems. 15 et al. ; , Osborne and Westrum Jr. ; the curve 6. The reduced enthalpy increment (in J K 1 mol 1) shows the recommended equation...... 53 29 1 1 of Nd2O3; ○, Blomeke and Ziegler ; &, King 16. The heat capacity (in J K mol ) of ThO2; , et al.27; , value derived from the low-temperature Ronchi and Hiernaut307; & Dash et al.325; the measurements by Justice and Westrum, Jr.;28 the curve shows the recommended equation. Note that curve shows the recommended equation...... 16 the data of Ronchi and Hiernaut307 indicate a value 7. The reduced enthalpy increment (in J K 1 mol 1) of about 600 J K 1 mol 1 (not shown in the graph) 115 of B-Sm2O3; ○, Gvelesiani et al. ; &, Pankratz at the maximum of the anomalie...... 54 114 112 340 et al. ; ~, Curtis and Johnson ; , value 17. The heat capacity of UO2.667; &, Inaba et al. ; derived from the low-temperature measurements &, Westrum Jr. and Grønvold342; ~, Girdhar and by Justice and Westrum Jr.113; the curve shows the Westrum Jr.339 ...... 55 recommended equation...... 19 18. The reduced enthalpy increment (in J K 1 mol 1) 1 1 336 8. The reduced enthalpy increment (in J K mol ) of UO2;○, Moore and Kelley ; &, Ogard and 374 375 of B-Eu2O3 (top) and C-Eu2O3 (bottom); ○, Gve- Leary ; ~ Fredrickson and Chasanov ; 5, lesiani et al.115; &, Pankratz and King128; ~;130 , Hein and Flagella376; ◊, Leibowitz et al.377; value derived from the low-temperature measure- (,378; , Mills et al.379; , value derived from the ments by Lyutsareva et al.126; the curves show the low-temperature measurements by Hunzicker and recommended equations...... 21 Westrum Jr.373; the curve shows the recommended 9. The reduced enthalpy increment (in J K 1 mol 1) equation...... 57 380 of B-Gd2O3 (top) and C-Gd2O3 (bottom); ○, Pank- 19. The heat capacity of UO2; ○, Ronchi et al. ; &, ratz and King128; &, Tsagareishvili et al.155; ~ Grønvold et al.349; ~ Amaya et al.381; 5, Popov Curtis and Johnson112; , value derived from the et al.335;◊, Hunzicker and Westrum Jr.373; (, Inaba low-temperature measurements by Justice and et al.382; the curve shows the recommended 113 Westrum Jr. for C-Gd2O3 and Konings equation...... 57 127 1 1 et al. for B-Gd2O3; the curves show the recom- 20. The reduced enthalpy increment (in J K mol ) 406 407 mended equations...... 23 of NpO2; &, Arkhipov et al. ; ◊, Nishi et al. ; 10. The reduced enthalpy increment (in J K 1 mol 1) ○, Beneš et al.408; , value derived from the low- 164 of Ho2O3; ○, Tsagareishvili and Gvelesiani ; &,28 temperature measurements by Westrum Jr. 58
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405 et al. ; the dashed curve shows the recommended 1. Introduction equation based on the estimates of Serizawa 410 et al...... The thermodynamic properties of the 4f (lanthanides) and 21. The reduced enthalpy increment (in J K 1 mol 1) 5f (actinides) elements and their compounds have been 421 419 of PuO2; ○, Ogard ; &, Kruger and Savage ; subject of many studies since the Second World War, strongly 5, Oetting422; , value derived from the low- stimulated by the demands of the nuclear technology. The temperature measurements by Flotow et al.420; development of nuclear reactor fuels based on uranium, the curve shows the recommended equation. . . . 59 thorium or plutonium and the understanding of the effects 22. The reduced enthalpy increment (in J K 1 mol 1) of fission product accumulation in the fuel, a significant 439 of AmO2 (&) and AmO1.5 (○) by Nishi et al. ; fraction of which belongs to the lanthanide group, required the solid curve shows the recommended equations, such fundamental data. At the same time, many studies of the the dashed curves the estimates based on compar- (thermodynamic) properties of the f-elements were stimu- ison with other lanthanide and actinide dioxides lated by the scientific interest in the role of the f-elements in and sesquioxides...... 61 the chemical bonding, and particularly the differences 23. The polymorphism of Ln2O3 (open symbols) and between the 4f and 5f series. An2O3 (closed symbols) compounds expressed Pioneering work on the major actinides has been performed as ionic radius versus temperature. The lines are during the Manhattan Project in the USA. The researchers in based on the transition temperatures in the this project started many systematic studies of uranium and lanthanide series (see Fig. 4)...... 86 plutonium and its compounds, the results of which became 24. The standard entropy S°(298.15 K) of the lantha- available in literature in the 1950s. At the meetings organised nide sesquioxides; ■ the lattice entropies derived in the frame of the Peaceful Uses of Atomic Energy initiative from experimental studies; & values calculated and also at the early Symposia on Thermodynamics of Nuclear from the lattice, represented by the dashed lines, Materials organised by the International Atomic Energy and excess entropy as explained in the text; ○ and Agency a rapid expansion of the knowledge of the thermo- the experimental values from the hexagonal/ dynamic properties of the actinide elements and their com- monoclinic and cubic compounds, respectively.. 86 pounds was presented. During the same period, the separation 25. The standard entropy S°(298.15 K) of the actinide methods for the lanthanides, which are difficult due to their sesquioxides; ■ the lattice entropies derived from chemical similarity, improved significantly to yield these experimental studies; & experimental value for elements in sufficient pure form that was needed for accurate 1,2 Pu2O3; ( estimated values from the lattice and thermochemical and thermophysical measurements. excess entropy as explained in the text...... 86 In the 1960s and 1970s a wealth of scientific information on 26. The enthalpy of the hypothetical solution reaction the f-elements has been published, the lanthanides as well as for the lanthanide (open symbols) and actinide uranium and thorium being available in pure form to many (closed symbols) sesquioxides, indicating the dif- researchers, and the other actinides being produced in sig- ferent structures (A-type, &; B-type, ~; C-type, nificant quantities for studies at nuclear research laboratories. ○)...... 86 As a result, the understanding of the trends and systematics of 27. The enthalpy of the hypothetical solution reac- their properties has improved considerably, revealing the tion for the lanthanide (open symbols) and acti- differences between the localised 4f electrons in the lantha- nide (closed symbols) sesquioxides as a function nides and the heavy actinides (Am-Lr) and the itinerant 5f of the molar volume, indicating the different electrons of the light actinides (Th-Np). structures (A-type, &;B-type,~;C-type,○).. 87 In this work, we will present a comprehensive review of the 28. The melting temperature (&, ■) and the enthalpies thermodynamic properties of the oxides of the lanthanides and of sublimation (○, ) of the actinide (open symbols) actinides, based on critical review of the available literature and lanthanide (closed symbols) dioxides...... 87 according to procedures described in Secs. 2.1–2.5. 29. The standard entropy S°(298.15 K) of the actinide dioxides; ■ the lattice entropies derived from experimental studies. The experimental value of 2. Approach CeO is also shown ( )...... 87 2 2.1. Thermal functions of condensed phases 30. The enthalpy of formation of the lanthanide(■)and actinide (&) dioxides...... 87 The approach adopted in this review is based on a critical 31. The enthalpy of formation of the actinide dioxides evaluation of the thermal functions (heat capacity, entropy, as a function of molar volume...... 88 enthalpy increment) and enthalpies of formation of the lantha- 32. The interatomic bond distance of the lanthanide ( ) nide and actinide oxides using, when possible, the primary and actinide (○) gaseous monoxides...... 88 experimental data as reported in literature. To describe these as 33. The dissociation enthalpy of the lanthanide (○) and a function of temperature it is necessary to include the data on actinide (&) gaseous monoxides...... 88 the structural transformations (including melting point).
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The reported transition and melting temperatures have been generally lacking to make the corrections properly, the experi- corrected to the International Temperature Scale ITS-90. mental enthalpy data have not been corrected. Though generally no detailed information is given about the All literature data starting from 1945 have been collected standards used and it is not specifically stated to which earlier systematically. When no experimental data were given in the temperature scales the data refer, it is assumed that the results papers, they have been extracted from digitalized graphs. between 1948 and 1968 refer to IPTS-48 and between 1969 and 1990 to IPTS-68. Especially in the transition years this 2.2. Enthalpies of formation of condensed phases may not always be correct. The differences between ITS-90 and IPTS-68 and IPTS-68 and IPTS-48 are shown in Fig. 1. The derivation of the enthalpies of formation from calori- The low-temperature heat capacity data and the resulting metric data was done by recalculation of the thermochemical entropies have not been corrected nor refitted. First, the reaction schemes (Hess cycles) using a consistent set of changes in the temperature scales in the range T ¼ (0 to auxiliary data, and has been partially reported in earlier work3 300) K are small, and, second, refitting would only marginally that was updated where necessary. For the solution calori- change the results. In case of more than one set of experimental metric studies the partial molar enthalpy of formation of an data covering the temperature range from close to 0 K to room acid solution (sln) at the concentration given, has been calcu- temperature, often a motivated choice for one of them is made, lated from the enthalpy of formation of the infinitely dilute based on sample purity and/or calorimetric accuracy. In other acid,4 the enthalpy of formation of the HX solutions5 and the cases a joint treatment has been made using overlapping densities of the HX solutions at 298.15 K,6 neglecting the polynomial equations. influence of the dissolved ions. Uncertainty limits of the The high-temperature heat capacity of the solid phases has measurements, as listed in the tables or text, are always the been obtained by refitting of the experimental data reported. values given in the original paper, because in many cases they The following polynomial equation for the enthalpy increment could not be recalculated due to lack of information. As a fH ðTÞ H ð298:15 KÞg has been adopted consequence they might refer to one standard deviation of the X mean, twice the standard deviation of the mean, or the 95% n fH ðTÞ H ð298:15 KÞg ¼ AnðT=KÞ ð1Þ confidence interval, which is not always clear. When combin- ing data from different sources to a selected value, a weighted with n ¼ 1 to 2, but in case of anomalous behavior of the heat mean is therefore considered not justified and the uncertainty capacity with n up to 4. This corresponds to a heat capacity limit of the selected (mean) value has been estimated. Aux- equation of the type iliary data recommended by CODATA or values consistent X 4 2 n with the CODATA selection have been employed. CpðTÞ¼a 2ðT=KÞ þ anðT=KÞ : ð2Þ
A difficult question to be answered is that of the temperature correction of high-temperature heat capacity and enthalpy 2.3. Thermal functions of gases data. As can be seen in Fig. 1 the temperature corrections Thermal functions of the diatomic molecules were calcu- become significant (>2 K) above 2000 K. For heat capacity lated in the present work using the approach developed by data, which are rare above this temperature, the correction is Gurvich et al.7 The vibrational-rotational partition functions straightforward, and has been made. However, for enthalpy were calculated by direct summation over vibrational levels increment data the corrections are not trivial as they depend on and by integration with respect to rotational levels. The upper the type of device used and the condition of the sample. In case limit of integration was assumed linearly decreasing with of the device was calibrated with a known standard (for vibrational quantum number. example, sapphire) the temperature correction should also be The electronic partition functions were calculated taking made for the standard, and hence not only the temperature but into account all experimentally known and estimated data on also the enthalpy conversion factor is affected. Also in case of excited states. The value of Qint and its derivatives were encapsulated samples the temperature correction should lead ðiÞ ðXÞ evaluated assuming that Q ¼ðp =p Þ . This approach to an enthalpy correction, as the contribution of the encapsula- vib;rot i X vib;rot is well justified in the case of the molecules under considera- tion material would change. Since the required details are tion though the most of these molecules have numerous low- lying states, which contribute considerably to the thermal 10 functions. The point is that these states as a rule belong to the same electron configuration as the ground state. It is well 5 T68-T48 known that the states of the same configuration have close
T/K values of vibrational and rotational constants. Therefore, the Δ 0 tables of molecular constants present the vibrational and T -T 90 68 rotational constants only for the ground state. The only excep- -5 tion is the YbO molecule for which the ground state config- 0 1000 2000 3000 4000 uration gives only one state, namely, the X1Σ state, while the T/K low-lying states belong to the other configurations with quite
FIG. 1. The temperature corrections according to various temperature scales. different molecular constants. The excited states are presented
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in the tables in two blocks for experimentally known and based on calculations with new thermal functions of these estimated states with corresponding statistical weights. The molecules, and to take into consideration new experimental uncertainties in the energies of experimental states are usually data and quantum chemical calculations not included in pre- small, but for estimated states they can amount to 10%–20% of vious assessments. the listed values. The recommended enthalpies of formation at the standard For simplification of introducing a huge number of high- temperature T ¼ 298.15 K have been selected in this review energy excited electronic states for molecules under consid- after critical analysis of all accessible published experimen- eration, containing f and d open shells, in the present work the tal data on high-temperature equilibriums for reactions in approach of the density of states estimation was applied. In this the gas phase or in condensed and gas phases. The enthalpies approach, a group of high-energy states with close energies are of reactions were calculated from the equilibrium constants united in one state with fixed (mostly rounded) energy and by the “second-law” and the “third-law” methods.7,9 By the average statistical weight. This division into groups of states is former, the enthalpy of reaction at the mean temperature of being done in a way that does not interfere with the accuracy of experiments Tmean is obtained from the temperature depen- the thermal functions calculation. Errors of the calculated dence of equilibrium constant, Kp,measuredinsometem- thermal functions depend mostly on the accuracy of the data perature interval: on molecular constants. At room temperature, the uncertain- 1 D H ðT Þ dðln K Þ ties in heat capacity as a rule do not exceed 0.3–0.5 J K r mean ¼ p : ð4Þ mol 1. At higher temperatures, the uncertainties become R dð1=TÞ larger because of the increasing contribution of excited states The value T is calculated using equation T and errors of these estimations. In heat capacity the uncertain- P mean mean 1 1 1 ties can reach 3–5 J K 1 mol 1 at 4000 K, or even larger for ¼ðn Ti Þ ,wheren is the number of experimental Δ molecules that entirely lack experimental data, such as PaO, points. The rH°(Tmean) value so obtained is reduced to the NpO, AmO, CmO, or PuO. reference temperature 298.15 K: The thermal function of the polyatomic molecules were
calculated using the rigid-rotor harmonic oscillator appro- Tmean 7,8 D H ð298:15 KÞ¼D H ðT Þ D fD H g: ð5Þ ach, that includes general approximations for the transla- r r mean r 298:15 tional, rotation and vibrational contributions, and a direct summation of the electronic partition function. In the “third-law” method, ΔrH°(298.15 K) is obtained from The heat capacity values were approximated by two con- every experimental Kp value jugated equations of the form: X D : D f ; = 2 = n: rH ð298 15 KÞ¼T r RTlnKp ð6Þ CpðTÞ¼a 2ðT KÞ þ anðT KÞ ð3Þ using the free energy functions (or reduced Gibbs energies) f, The accuracy of the approximation is around 0.1 J K 1 mol 1 which is defined as over full temperature range from 298.15 to 4000 K. The nomenclature used in the tables of molecular properties of the gaseous species is summarized in Table 1. The funda- f ¼ fG ðTÞ H ð298:15 KÞg=T; ð7Þ mental constants as recommended by CODATA are used in this work. T D : H ¼ S ðTÞ 298 15 ; ð8Þ T 2.4. Enthalpies of formation of gases for each reactant. The enthalpy of formation for the molecule The aim of this review is to select the most reliable under study, ΔfH°(298.15 K) is calculated from the enthalpy of enthalpies of formation for MO, MO2, and MO3 molecules a reaction using known enthalpies of formation for all other reactants. Δ TABLE 1. Nomenclature of the molecular properties for the di- and polyatomic The uncertainties ascribed to selected fH°(298.15 K) species values reflect statistical errors, uncertainties in the thermal Symbol Name Symbol Name functions, and uncertainties in enthalpies of formation for all other reaction participants. Most experimental measure- Te Electronic energy level σ Symmetry number p Degeneracy (of Te)IAIBIC Product of moments ments for equilibriums involving the considered molecules of inertia were carried out by Knudsen effusion (KE) and mass ω n e Fundamental harmonic i Fundamental spectrometric methods (MS), or by combination of both. vibrational frequency vibrational frequency In the case of MS measurements, the term RT ln(1.5) was ω x Anharmonicity correction e e added to reflect uncertainties of equilibrium constants cal- be Rotational constant ae Rotational-vibration culated from ion currents, due to uncertainties in ionization interaction constant cross sections. Agreement of the second- and third-law De Centrifugal distortion values was regarded as an indication of reliability of experi- constant mental data.
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2.5. Consistency and completeness TABLE 2. Temperature of melting of lanthanum sesquioxide (after Coutures and Rand15) We have tried to maintain the internal consistency of the recommended data as much as possible, but in view of the Tfus/K complex interrelationships in some of the analysed systems Authors Reported ITS-90 (e.g., Ce-O, U-O or Pu-O) and the fact that data from Wartenberg and Reusch16 2588 2581 other sources have been used this cannot be fully guaranteed. Lambertson and Gunzel17 2483 20 2489 20 18 The review has been performed progressively during a period Sata and Kiyoura 2577 2 2583 2 Foex19 2573 2587 of several years. New information that became available Mordovin et al.20 2493 30 2496 30 during and just after this period has been incorporated as far Noguchi and Mizuno21 2530 20 2532 20 as possible, but in some cases the implications of adopting new Treswjatskii et al.22a 2583 20 2582 20 (more accurate) values were too far-reaching to be implemen- Coutures et al.23 2593 10 2592 10 12 ted. These cases are clearly identified in the text. Wehner et al. 2563 30 Mizuno et al.24 2569 20 2555 20 Yoshimura et al.25 2573 5 2576 5 3. The Lanthanide Oxides in Solid and Shevthenko and Lopato13 2583 2582 Ushakov and Navrotsky14 2574 10 Liquid State Selected value: 2577 15 aAlso reported by Lopato et al.11 3.1. La2O3(cr,l) 3.1.1. Polymorphism and melting point temperature the differences significantly increase. The Lanthanum(III) oxide has a A-type hexagonal sesquiox- selected standard entropy of La2O3 has been derived from the ide structure (space group P3m1) at room temperature. It measurement by Justice and Westrum, Jr.,28 which is con- transforms to a H-type hexagonal structure upon heating. sidered to be the most accurate Foex and Traverse10 suggest that this transformation is a simple displacement rearrangement of the lattice,10 as in a → S ð298:15 KÞ¼ð127:32 0:84Þ JK 1 mol 1: b quartz. Foex and Traverse,10 Lopato et al.11 and Wehner 12 → The high-temperature enthalpy increment of La2O3(cr) et al. all reported the A H transition at T ¼ 2313 K, 29 13 14 has been measured by Blomeke and Ziegler from 380 to Shevthenko and Lopato at T ¼ 2303 K, and at (2319 5) 27 30 K. The H phase subsequently transforms into a cubic X-type 1170 K, King et al. from 399 K to 1797 K, Yashvili et al. from 380 to 1650 K and Sedmidubský et al.31 from 689 to structure (space group Im3m) and the transformation tem- 1291 K, which are in perfect agreement, as shown in Fig. 2. peratures were reported as T ¼ 2383, 2413, 2363, and 2373 K, The measurements smoothly join the low-temperature heat (2383 5) K, respectively. Except for the recent work by 28 14 capacity measurements by Justice and Westrum, Jr. Basili Ushakov and Navrotsky, all other measurements must et al.32 measured the heat capacity of La O from 400 to be converted to ITS-90. The measurements of Foex and 2 3 10 850 K. Their results, only presented in graphical form, Traverse must be corrected by +14 K, following the pro- 15 11 reasonably agree with the enthalpy measurements to about cedure outlined by Coutures and Rand. Lopato et al., 12 13 550 K. The heat capacity above 298.15 K for A-type La O Wehner et al., and Shevthenko and Lopato reported no 2 3 canberepresentedbytheequation(298.15to1800K): (detailed) information on the calibration of their measure- ments, but assuming the data refer to IPTS-68, a correction = 1 1 : : 3 = CpðTÞ JK mol ¼ 120 6805 þ 13 42414 10 ðT KÞ of 1 K needs to be applied. We select Ttrs ¼ (2313 30) K 14:13668 105ðT=KÞ 2 for the A → H transformation, Ttrs ¼ (2383 30) K for the H → X transformation. Various measurements of the melting temperature of solid La2O3 have been reported as summarized in Table 2,which is based on the IUPAC review by Coutures and Rand;15 150 the results being corrected to ITS-90. The recent value for 14 the melting by temperaturebyUshakovandNavrotsky 125 is in excellent agreement with the selected values by Cou- (298.15 K) tures and Rand,15 and the latter is retained, T ¼ (2577 o fus 100 (T - 298.15)