Category Archives: An Introduction to Nuclear Materials

Hydrostatic and Deviatoric Stresses

Total stress tensor can be divided into two components: hydrostatic or mean stress tensor (om) involving only pure tension or compression and deviatoric stress tensor

image643 Подпись: (A. 8a) (A.8b)

(o’j) representing pure shear with no normal components:

It is to be noted that pure hydrostatic stress does not lead to plastic deformation and finite deviatoric stresses are needed for any plastic deformation to take place.

A.4

Normal and Shear Stresses on a Given Plane (Cut-Surface Method)

Given Oj in reference system 12 3, n is the unit vector normal to the plane = njn2n3, m is the unit vector in the plane = m1m2m3, oN is the normal stress along n, and t is the shear stress along m (see Figure A.2).

Note: П ■ m — 0, n2 + n2 + n| = 1, and m1 + m2 + m2 = 1. If П — 1, 2, 5 ) П — 1/^30, 2Д/30, 5Д/30 , n is a unit vector, where /12 + 22 + 52 = /30 so that n1 + n2 + n2 = 1.

First, we find the stress vector (S) {the stress vector is the vector force per unit area acting on the cut}:

S1

011

012

013

S2

— 021

022

023

S3

031

032

033

n1 3^

n2 ) Si = Oikm;

n3 k=1

that is, S1 = o11n1 + o12n2 + o13n3, and so on. oN and t are given as follows: oN = S ■ n = S1n1 + S2n2 + S3n3 and

Подпись:

image646

t — S ■ m = S1m1 + S2m2 + S3m3,

Figure A.2 Designations for normal and shear stress calculations.

image647

and tmax occurs when n, S, and m are in the same plane:

Thus, given the stress tensor, we need only two elastic constants E and n, since G is related to E and n:

G = E/2(1 + n). (A. 14)

We now note that the volume change or dilatation is given by

Д =(1- + e1)(1 + e2)(1 + e3) — 1 — e1 + e2 + e3

since e’s << 1. Note that Д is the first invariant of the strain tensor and mean strain em = Д/3.

image648

Thus, bulk modulus

(A.17)

Note that the derivative of U0 with respect to any strain component equals the cor­responding stress component:

Подпись: dU0 dsx — 1Д T 2Gex — Sx

image650 Подпись: '-x •

and similarly

A.7

Generalized Hooke’s Law

Подпись: (A. 18)Подпись: (A. 19)eij Sijklakl:

Here Sjki is the elastic compliance tensor (fourth rank) and

aij Cijklekh

where Cijkl is elastic stiffness (or elastic constants).

Crystal symmetry reduces the number of independent terms: cubic — 3, hexago­nal — 5, and so on, and these are related to E and G.

Details on these compliance and stiffness coefficients are beyond the scope of this book and may be found elsewhere.

image652

Appendix B

B.1

SI Units

Quantity

Unit

Symbol

Length

Meter

m

Mass

Kilogram

kg

Time

Second

s

Electric current

Ampere

A

Temperature

Kelvin

K

Amount of substance

Mole

mol

Luminous intensity

Candela

cd

Plane angle

Radian

rad

Solid angle

Steradian

sr

B.2

Some Derived Units

Quantity

Special

name

Symbol

Equivalence in

Other Base derived units units

Force, load, weight

Newton

N

kgm s-2

Stress, strength, pressure

Pascal

Pa

N m-2

kgm-1 s-2

Frequency

Hertz

Hz

s-1

Energy, work, heat

Joule

J

Nm

kg m2 s-2

Power

Watt

W

Js-1

kg m2 s-3

Electric charge

Coulomb

C

A s

Electric potential/voltage

Volt

V

WA-1

kg m2 s-3 A-1 (continued)

An Introduction to Nuclear Materials: Fundamentals and Applications, First Edition.

K. Linga Murty and Indrajit Charit

© 2013 Wiley-VCH Verlag GmbH & Co. KGaA. Published 2013 by Wiley-VCH Verlag GmbH & Co. KGaA.

Quantity

Special

name

Symbol

Equivalence in

Other Base derived units units

Resistance

Ohm

V

VA-1

kgm2s-3 A-2

Capacitance

Farad

F

C V-1

kg-1 m-2 s4A2

Magnetic flux

Weber

Wb

Vs

kgm2 s-2 A-1

Magnetic flux density

Tesla

T

Wb m

-2

kgs-2 A-1

Inductance

Henry

H

Wb A-

1

kg m2 s-2 A-2

B.3

Standard Unit Prefixes and Their Multiples and Submultiples

Name

Multiplication factor

Symbol

Atto

10-18

a

Femto

10-15

f

Pico

10-12

p

Nano

10-9

n

Micro

10-6

m

Milli

10-3

m

Kilo

103

k

Mega

106

M

Giga

109

G

Tera

1012

T

B.4

Some Unit Conversion Factors

B.4.1

Length

1 inch = 25.4 mm 1 nm= 10-9m 1 mm = 10-6 m 1A= 10-10m = 0.1 nm

B.4.2

Temperature

T (K) = T (°C) + 273.15 T (°C) = [T (°F) — 32]/1.8

B.4.3

Mass

1 Mg= 103kg 1kg = 10~3 Mg

1kg = 103g 1kg = 2.205 lbm

1g = 10~3kg

B.4.4

Force

1kgf = 9.81 N 1lb = 4.448 N 1 dyne = 10~5 N

B.4.5

Stress

1 ksi (i. e., 103 psi) = 6.89 MPa 1 MPa= 1N mm-2 = 145 psi 1Pa = 10 dyn cm-2 1 ton in.-2 = 15.46 MPa 1 atm = 0.101325 MPa 1bar = 0.1 MPa 1 Torr (mmHg) = 133.3 MPa

B.4.6

Energy, Work, and Heat

1 eV atom 1 = 96.49 kJ mol 1 1 cal = 4.184 J 1 Btu = 252.0 cal 1 erg = 10-7 J

B.4.7

Miscellaneous

1° = rad

57.3

Подпись:1 g cm-3 = 1000 kg m~3 1 poise = 0.1 Pas 1 ksi in.1/2 = 1.10 MN m~3/2

B.5

Selected Physical Properties ofMetals (Including Metalloids)

Symbol

Atomic

number

Atomic

weight

Density at 20 °C (gcm-3)

Melting point (°C)

Al

13

26.98

2.7

660

Sb

51

121.76

6.68

630.5

As

33

74.91

5.727

814

Ba

56

137.36

3.5

710

Be

4

9.013

1.845

1284

Bi

83

209.0

9.8

271.2

B

5

10.82

2.34

2300

Cd

48

112.41

8.65

320.9

Ca

20

40.08

1.54

851

Ce

58

140.13

6.66

795

Cs

55

132.91

1.873

28.5

Cr

24

52.01

7.19

1875

Co

27

58.94

8.90

1493

Nb

41

92.91

9.57

2468

Cu

29

63.54

8.94

1083

Dy

66

162.51

8.536

1407

Er

68

167.21

9.051

1497

Eu

63

152.0

5.259

826

Gd

64

157.26

7.895

1312

Ga

31

69.72

5.907

29.75

Ge

32

72.60

5.32

936

Au

79

197.2

19.32

1063

Hf

72

178.50

13.29

2150

Ho

67

164.94

8.803

1461

In

49

114.82

7.31

156.6

Ir

77

192.2

22.42

2410

Fe

26

55.85

7.87

1535

La

57

138.92

6.174

920

Pb

82

207.21

11.34

327.4

Li

3

6.940

0.534

179

Lu

71

174.99

9.842

1652

Mg

12

24.32

1.74

651

Mn

25

54.94

7.44

1244

Hg

80

200.61

13.55

-38.87

Mo

42

95.95

10.22

2610

Nd

60

144.27

7.004

1024

Ni

28

58.69

8.9

1452

Os

76

190.2

22.5

3000

Pd

46

106.4

12.02

1552

(continued)

Symbol

Atomic

number

Atomic

weight

Density at 20 °C (gcm~3)

Melting point (°C)

Pt

78

195.09

21.40

1769

Pu

94

239.11

19.84

639.5

K

19

39.10

0.87

63.7

Pr

59

140.92

6.782

935

Pm

61

145

7.264

1035

Re

75

186.22

21.02

3180

Rh

45

102.91

12.44

1960

Ru

44

101.1

12.4

2250

Sm

62

150.35

7.536

1072

Sc

21

44.96

2.99

1539

Se

34

78.96

4.79

217

Si

14

28.09

2.33

1410

Ag

47

107.873

10.49

960.5

Na

11

22.991

0.97

97.9

Sr

38

87.63

2.6

770

Ta

73

180.95

16.6

2996

Te

52

127.61

6.25

449.5

Tb

65

158.93

8.272

1356

Tl

81

204.39

11.85

303

Th

90

232.05

11.66

1750

Tm

69

168.94

9.332

1545

Sn

50

118.7

7.3

232

Ti

22

47.90

4.54

1668

W

74

183.92

19.3

3410

U

92

238.07

19.07

1132

Yb

70

173.04

6.977

824

Y

39

88.92

4.472

1509

Zn

30

65.38

7.133

419.5

Zr

40

91.22

6.45

1852

Adapted from Ref. [1].

B.6

Thermal Neutron (0.025 eV) Absorption Cross Sections of Some Elements

Element

Absorption

cross

section (b)

Element

Absorption

cross

section (b)

Element

Absorption

cross

section (b)

C

0.0035

Ni

4.49

Ho

64.7

Be

0.0076

Sb

4.91

Lu

74

Bi

0.034

V

5.08

Am

75.3

Mg

0.063

Ti

6.09

Re

89.7

Si

0.171

Pd

6.90

Au

98.7

Pb

0.171

Th232

7.56

Tm

100

Zr

0.185

U

7.57

Hf

104.1

Al

0.231

La

8.97

Rh

144.6

H

0.332

Pt

10.3

Np

175.9

Sn

0.626

Pr

11.5

Er

159

Ce

0.630

Se

11.7

In

193.8

Zn

0.110

Mn

13.3

Pu240

289.6

Nb

1.15

Os

16.0

Ir

425

Y

1.28

W

18.3

B

767

Ge

2.20

Ta

20.6

Dy

994

Fe

2.56

Tb

23.4

Pu239

1017.3

Ru

2.56

Sc

27.5

Pu241

1400 (*)

Mo

2.48

Co

37.2

Cd

2520

Cr

3.05

Yb

34.8

Eu

4530

Tl

3.43

Nd

50.5

Sm

5922

Cu

3.78

Ag

63.3

Gd

49 700

Te

4.7

[Source: Special feature section of neutron scattering lengths and cross sections of the elements and isotopes, Neutron News, 3 (1992) 29-37]

B.7

Mechanical Properties of Some Important Metals and Alloys

Alloy

Young’s

modulus

(GPa)

Poisson’s

ratio

UTS

(MPa)

YS

(MPa)

Elongation

to

fracture (%)

Fracture toughness (MPa m1/2)

Al 2024 T851

72.4

0.33

455

400

5

26.4

Al 7075 T651

72

0.33

570

505

11

24.2

Al 7178T651

73

0.33

605

540

10

23.1

Ti-6Al-4V

113.8

0.342

1860

148

14

55

(grade 5)

Alpha annealed

100

0.3

620

500

15

100

Ti-3Al-2.5V

702 Zirconium

99.3

0.35

379

207

16

Stainless steel

205

745

470

22

60.4

4340

Stainless steel

193

0.29

505

215

70

304

Tool steel H11

210

1990

1650

9

(hot worked)

Maraging steel

200

1864

1737

17.4

Superalloy

860

310

10

CoCrWNi

Superalloy H-X

690

276

40

nickel

B.8

Mechanical Properties of Some Important Ceramics

Ceramic

Young’s

modulus

(GPa)

Poisson’s

ratio

Hardness

(HV)

Tensile

strength

(MPa)

Compressive

strength

(MPa)

Flexural

strength

(MPa)

Fracture toughness (MPa m1/2)

Silicon

nitride

320

0.28

1800

350-415

2100-3500

930

6

Silicon

carbide

450

0.17

2300

390-450

1035-1725

634

4.3

Tungsten

carbide

627

0.21

1600

344

1400-2100

1930

MgO-stabilized

ZrO2

200

0.3

1200

352

1750

620

11

Boron

carbide

450

0.27

2700

470

450

3.0

Titanium

diboride

556

0.11

2700

470

277

6.9

Note: The above values are indicative only. Adapted from Ref. [2].

Подпись: 1 Hampel, C.A. (1961) Rare Metals Handbook, Chapman & Hall, London. Подпись: 2 Meyers, M.A. and Chawla, K.K. (2009) Mechanical Behavior of Materials, Cambridge University Press.

References

[1] For example, B10 + n1 ! Li7 + He4.

[2] Using these data, evaluate the parameters n and Q in the power-law creep equation.

ii) Identify the underlying creep mechanism.

iii) If in another example, a thin polycrystalline sample exhibited essentially the same n and Q, what would be the controlling creep mechanism?

[3] Relaxation (or excess) volume is generally asso­ciated with a defect leading to some form of internal stress and is expressed in terms of atomic volume (V). Relaxation volume basi­cally measures the distortion volume induced in the lattice due to the insertion of a vacancy or interstitial. Most calculations of relaxation

Radiation Swelling

Irradiation swelling is a type of dimensional instability (in the form of volume expansion) that is encountered through the formation of voids/bubbles and fission

image599

image600

Figure 7.8 Radiation growth effect (length increase) in an irradiated uranium fuel specimens rolled at 600 °C as a function of fuel burnup. Adopted from Ref. [2].

 

image601

image602
image603

20 —

 

15 —

 

4000

 

2000

 

5000

 

image604

image241

FUEL BURNUP (MWD/T)

Figure 7.9 The extent of swelling in various uranium-based materials as a function of fuel burnup. Taken from Ref. [2].

not in gamma-uranium, while both phases can exhibit radiation swelling even though alloying may minimize the radiation swelling effect.

Figure 7.9 shows the volume change as a function of fuel burnup for a number ofuranium-based materials. This does show the effect of alloying in suppressing radi­ation swelling. Note that the adjusted uranium shown in the plot is known as the Brit­ish Standard Fuel Produce (contains 400-1200ppm, 300-600ppmC, and small amounts ofMo, Nb, and Fe) and it shows better radiation swelling performance.

image605

Figure 7.10 Thermal creep and irradiation creep curves of hot rolled uranium under differently processed conditions — 1: Beta-cooled in air, 2: beta-quenched in water, 3: gamma-cooled in air, 4: gamma-quenched in water; after Ref. [2].

Irradiation Creep

Creep is an important time-dependent mechanical property for high-temperature application. In Chapter 6, we have learned how thermal creep is different from irradiation creep. So, here we are not going to repeat the fundamental principles. Figure 7.10 shows the effect of irradiation on the creep behavior of hot rolled uranium.

7.2.2

Fluence Dependence ofVoid Swelling

We have already observed the effect of fluence in Figure 6.18 on the void swelling behavior of austenitic stainless steels like 316 type. It has been observed that the swelling extent increases with increasing neutron fluence (or dpa) and empirical relations have also been developed. It has been noted that there exists an incubation period that represents the neutron dose needed to produce enough helium and point defect concentration to make void nuclea — tion possible. The incubation period may also be needed to develop enough number of interstitial dislocation loops to allow the preferred absorption of interstitials by dislocations to sufficiently bias the point defect population in the material in favor of vacancies as to permit vacancy agglomeration into voids. However, incubation period does depend on temperature and material/ microstructure. Figure 6.20 shows a generalized form of void swelling behav­ior as a function of dose or fluence. The initial transient period is followed by a steady-state swelling period. This steady-state period for FCC-based materials continues to proceed with no sign of saturation. However, void swelling in BCC-based metals/alloys (like F-M steels) shows saturation effect. In these systems, at higher radiation doses, voids/bubbles self-organize following the crystallography of the metal leading to void/bubble lattices.

image529

Figure 6.20 Generalized void swelling behavior as a function of radiation dose, showing different stages.

Подпись: Note Radiation growth is another radiation effect that occurs in materials with anisotropic structure or strong texture. Radiation growth does not lead to change in volume as the void swelling, but rather conserves the volume. It has been observed in zircaloys (HCP crystal structure) and alpha-uranium (orthorhombic). It is easier to think of a single crystal of alpha-Zr to understand the radiation growth effect. The c/a ratio of the crystal decreases or the single crystal becomes short and fat, thus conserving the volume. The length increase of fuel rod under irradiation can occur if the crystallographic texture of the zircaloy is such that the a-axis of the crystals is oriented near to the length axis. This effect is further discussed in Chapter 5 with respect to radiation growth effect seen in uranium.

6.1.3

Radiation-Induced Segregation

Radiation-induced segregation (RIS) involves segregation of alloying elements under fast particle irradiation to certain microstructural locations leading to a situa­tion where otherwise homogeneous alloys become heterogeneous. During fast par­ticle irradiation, significant diffusion fluxes of point defects (vacancies and interstitials) can be set up in the vicinity of the defect sinks like surfaces or internal grain boundaries. Generally, we have come to know from Section 2.3 that the differ­ent atomic species in an alloy migrate at different rates in response to the already set up point defect fluxes so that some species travel toward the said defect sinks while others move away. Thus, RIS can lead to significant alterations in the local composition near the sinks like grain boundaries, and this can have substantial bearing on the macroscopic properties of the materials. This phenomenon has been studied in some detail, particularly in structural materials used in nuclear reactor components. Understanding RIS is of particular importance in chromium containing austenitic stainless steels or nickel base superalloys because these alloys are used in commercial power reactors and potential candidate materials for advanced reactors. RIS can potentially lead to irradiation-induced stress corrosion cracking as chromium segregates away from the grain boundaries where it is most needed. At low temperatures, defect concentration builds up and rather than going to the sinks, point defects tend to recombine. At higher temperatures, thermal dif­fusion dominates and composition becomes equilibrated or homogeneous. At intermediate temperatures, RIS becomes acute due to the operation of a process known as “inverse Kirkendall” effect. Figure 6.21 shows the composition profile in an irradiated 300 series stainless steel, analyzed by energy dispersive spectroscopic measurement conducted with a JEOL 2010F high-resolution transmission electron microscope, showing depletion of Cr and enrichment of Ni, Si, P at the grain boundary due to RIS.

image531

Figure 6.21 Radiation-induced segregation of Cr, Ni, Si, and Pat the grain boundary of a 300 series stainless steel irradiated in a LWR core to several dpas at 300°C [19].

6.1.4

Radiation Effects

Thorium has cubic crystal structure and is thus isotropic. It does not show radia­tion growth effect and thus has better dimensional stability than a-U under irradiation.

7.2.3.1 Pros and Cons ofThorium-Based Fuel Cycles

Thorium is more abundant in nature compared to uranium and naturally there is interest in having an economic fuel cycle based on thorium. Thorium-based fuel cycles offer attractive features that are low level of waste generation along with a less amount of transuranics in the waste and provide a robust diversification option for nuclear fuel supply. Also, the use of thorium in majority of reactors leads to significant additional safety margins. However, the full commercial exploitation of thorium fuels has some significant obstacles in terms ofbuilding an economic case to undertake the necessary developmental work. A great deal of R&D, testing, and qualification work is required before any thorium fuel can be considered for rou­tine commercial application. Other obstacles to the development of thorium fuel cycle are the greater fuel fabrication and reprocessing costs to include the fissile plutonium as a driver material. The high cost of fuel fabrication is partly because of the high level of radioactivity that is involved in the presence of U-233, chemi­cally separated from the irradiated thorium fuel. But the U-233 gets contaminated with traces of U-232 that decays (69-year half-life) to daughter nuclides such as thal­lium-208 that are high-energy gamma-emitters [14]. Even though this improves the proliferation resistance of the fuel cycle, it also makes U-233 hard to handle and easy to detect. Notwithstanding, thorium fuel cycle provides hope for long-term energy security benefits without the need for fast reactors.

Metallic fuels with their high neutron economy, good thermal conductivity, and thermal shock resistance should be the natural choice for fuels. However, they are not adequate for high-temperature reactors due to low strength at high temperatures, phase transformations, and so on. The other ceramics have superior strength at higher temperatures, low thermal expansion, good corro­sion resistance, and good radiation stability. A wide range of compounds are considered as ceramics, which include oxides, carbides, nitrides, borides, sili — cides, sulfides, selenides, and so forth. But ceramics also suffer from brittle­ness especially at lower temperatures. Here, we will discuss few ceramic nuclear fuels and discuss their salient features.

7.3.1

Radiation Effect on Fatigue Properties

Here, we will only briefly discuss the effect of radiation on fatigue properties. Recall the universal slopes method in Section 5.1, given by

Де = ANf 0:6 + BNf 0:12, (6.15)

where the first term represents the low cycle fatigue (LCF) that is controlled by ductility, while the second term represents high cycle fatigue (HCF) controlled

О to’1

image562
Подпись: creep
image564
Подпись: Dislocation
Подпись: 024
Подпись: N-H
Подпись: 650 C

image5690.2 0.4 0.6 0.8

Подпись: Figure 6.40 Deformation mechanism map of an irradiated 316-type stainless steel [34]. Nf

Normalized Temperature, T/TM

Figure 6.41 Effect of neutron radiation exposure on fatigue of 304-type stainless steel [35].

by strength. Now we know the constant A is directly proportional to ductility (i. e., reduction in area), while the constant B is proportional to strength (such as ulti­mate tensile strength). Since radiation exposure leads to hardening and embrittle­ment, fatigue life decreases in LCF and increases in HCF. Figure 6.41 illustrates the features clearly delineated in irradiated stainless steel tested at 325 °C, where it is noted that radiation exposure results in decreased fatigue life in LCF while improved life in HCF.

6.3

Nuclear Fuels

“We believe the substance we have extracted from pitch-blende contains a metal not yet observed, related to bismuth by its analytical properties. If the existence of this new metal is confirmed we propose to call it polonium, from the name of the original country of one of us.”

—Marie Curie

7.1

Introduction

The heart of a nuclear reactor is the “reactor core” that contains nuclear fuels among other components/materials. Nuclear fuel forms consist of radioactive materials that may create the fission chain reaction under suitable conditions creat­ing a large amount of heat that is then utilized for producing the electrical power. The following are the basic requirements of a nuclear fuel:

a) The capital installation costs for nuclear power plants are substantial. In order to maintain profitability in the power production, the fuel costs must be minimal.

b) Adequate thermal conductivity of nuclear fuels is necessary to ensure that they can withstand the thermal gradients generated between the fuel center and periphery.

c) The fuel should be able to resist repeated thermal cycling due to the reactor shutdowns and start-ups.

d) It should have adequate corrosion resistance against the reactor fluids.

e) It should transmit heat quickly out of the fuel center.

f)The fuel should be relatively free from the constituent elements or impurities with high neutron capture cross section in order to maintain adequate neutron economy.

g) It must be able to sustain mechanical stresses.

h) The fuels should be amenable for reprocessing or disposal.

Nuclear fuel materials developed over decades include metals/alloys (uranium, pluto­nium, and thorium) and ceramics (oxides, carbides, nitrides, and silicide compounds containing the former radioactive elements). Nuclear fuels are fabricated in a wide

An Introduction to Nuclear Materials: Fundamentals and Applications, First Edition.

K. Linga Murty and Indrajit Charit.

© 2013 Wiley-VCH Verlag GmbH & Co. KGaA. Published 2013 by Wiley-VCH Verlag GmbH & Co. KGaA.

variety of configurations, such as cylindrical pellets, long extruded rods (for metal/alloy fuels only), spherical particles, coated particles, dispersion fuels (such as cermets), and fluid forms (for aqueous homogeneous reactors and molten salt cooled reactors).

 

Some Basic Terms Regarding Nuclear Fuels

Burnup: Fuel burnup is an important property of nuclear fuels. Burnup is gener­ally defined as the amount of heavy metal (in the form of uranium and higher actinides) in the fuel that has been fissioned. This term can be expressed either as a percentage of heavy metal atoms that have fissioned (atom%) or in units of fission energy (gigawatt-day or GWd; 1 GWD = 8.64 x 1013 MWd) produced per metric ton of the heavy metal (MTHM), that is, GWd/MTHM or MWd/kgHM. One atom% burnup corresponds to approximately 9.4 GWd per MTHM. However, the fuel burnup is often limited by the fuel cladding per­formance. Superior cladding performance allows higher burnups in fuels. Blanket fuel: Nuclear reactor fuel that contains the fertile isotopes that are bred into fissile isotopes

Driver fuel: Nuclear reactor fuel that contains the fissile isotopes along with fer­tile isotopes that are bred into fissile isotopes Reproduction factor: It is generally represented by g, which is the number of neu­trons created per neutron absorbed in fuel. If v neutrons are produced per fission reaction, the number ratio of fission to absorption in fuel is of/oa and the number of neutrons per absorption is

sf

g = — v. (7.1)

sa

The value of g is higher in fast reactor compared to that in thermal reactors. Conversion ratio: The ability to convert fertile isotopes into fissile isotopes can be measured by the conversion ratio (CR) defined as

CR = Fissile atoms produced/fissile atoms consumed. (7.2)

If CR is >1 such as in a fast reactor, it is called the breeding ratio (BR). The breeding gain (BG) is given by (BR — 1), which represents the additional pluto­nium produced per atom burned.

Fission products (Fp): According to Kleycamp [1], the fission products can be classified as follows — (1) fission gases (fg) and other volatile elements — Br, Kr, Rb, I, Xe, Cs, and Te; (2) fission product forming precipitates — Mo, Tc, Ru, Rh, Pd, Ag, Cd, In, Sn, Sb, Se, Te; (3) Fp forming oxide precipitates — Rb, Sr, Zr, Nb, Mo, Se, Te, Cs, and Ba; and (4) Fp dissolved as oxides in fuel matrix — Rb, Sr, Zr, Nb, La, Ce, Pr, Nd, Pm, Sm, and Eu.

Fissium (Fs) or fizzium (Fz): Fissium is nominally 2.4wt% Mo, 1.9wt% Ru, 0.3 wt% Rh, 0.2wt% Pd, 0.1 wt% Zr, and 0.01 wt% Nb and is designed in such a way that it can mimic noble metal fission products remaining after a simple reprocessing technique based on melt refinement.

 

The history of metallic nuclear fuels dates back to the first developmental stages of nuclear reactors. U — and Pu-based fuels were used in the Experimental Breeder Reactor-1 (i. e., EBR-1) that produced useful electricity for the first time in December 1951. In addition, EBR-2, the first-generation Magnox reactors (such as Calder Hall in the United Kingdom), and many other subsequent fast reactors have used metallic fuels. When water-cooled reactors were being devel­oped, the metallic fuels were not chosen mainly because of the compatibility issues between water and metallic fuel at elevated temperatures arising during the event of a cladding breach resulting in the formation of metal hydrides or oxides. However, in the mid-1960s, when the fast reactor development was gain­ing ground, designers chose oxide fuels in place of metallic fuels as they envi­sioned that the metallic fuels would have only limited burnups because of the presumed swelling problems and anticipated creation of liquid phases in fuels during the higher temperature operations. During that time, oxide fuels were recommended for power reactors even though limited information was available on them. Later simple design changes for the fuel elements, widening the gap between the fuels and cladding materials and providing a plenum volume for accumulating fission gases, have shown marked improvement (1% versus 20% burnup) over the earlier designs where there was no gap or very little gap between the fuel and the cladding materials. However, it is important to note that research and test reactors have traditionally used metallic fuels mainly because of the lower temperature operations involved.

Here we highlight three main metallic nuclear fuel materials. Metallic fuels have a number of advantages as well as disadvantages often specific to the fuel types. However, the metallic fuels generally have higher thermal conductivity, high fissile atom density (improved neutron economy), and fabricability as their prime advan­tages, whereas lower melting points, various irradiation instabilities, poor corro­sion resistance in reactor fluids, and various compatibility issues with the fuel cladding materials are some prominent disadvantages. Metallic fuels can also be used in alloy forms to improve corrosion resistance and irradiation performance among others.

7.2.1

Metallic Plutonium

Plutonium (atomic number 94) and its alloys can be used as nuclear fuels in nuclear reactors and space batteries. Notably Pu239 is the major fissile isotope of plutonium. Among them, plutonium (Pu239) serves as a fissile fuel as its fission cross section is high (742.5 b) with thermal neutrons. Pu241 isotope also has signifi­cant fission cross section in the thermal spectrum (1009 b), whereas Pu240 can act as burnable poison allowing reactor to have constant reactivity throughout reactor lifetime. Plutonium is found in natural uranium only in trace quantity. It is mainly produced artificially by the transmutation reaction of U238 isotope (fertile fuel) with a neutron as described in Eq. (1.2). Radioisotopic thermoelectric generators also use plutonium (Pu238) to power spacecrafts. Plutonium appears originally as a bright silvery-white metal, but soon loses its bright color when oxidized in air. Smaller critical mass of plutonium (almost one-third of that of uranium), its high toxicity, and pyrophoricity warrant safe handling of this metal. Plutonium can be recovered from the spent fuel of a thermal reactor through chemical treatment. However, depleted uranium can be kept together with plutonium for fuels used in fast breeder reactors such as LMFBRs. In other cases, separated plutonium can be used in plutonium-burning reactors.

Hecker [5] noted the following in his paper about plutonium:

“PLUTONIUM is a notoriously unstable metal — with little provocation, it can change its density by as much as 25 pct; it can be as brittle as glass or as malleable as alumi­num; it expands when it solidifies; and its silvery freshly machined surface will tar­nish in minutes, producing nearly every color in the rainbow. In addition, plutonium’s continuous radioactive decay causes self-irradiation damage that can fundamentally change its properties over time.”

As we present in the next several sections various characteristics of plutonium, we must bear in mind this fickle nature of plutonium.

Radiation-Induced Precipitation or Dissolution

At intermediate temperatures and radiation doses of >10dpa, RIS effect may, in fact, lead to phase instability, involving precipitation of new phases or dissolution of existing phases. In Ni-Si system, Si as an undersize solute (atomic radius: 110 pm) compared to Ni (atomic radius: 135 pm) enriches the sinks, and when conditions are ripe, the solubility of Si in Ni exceeds the level forming new phase Ni3Si (y’-type structure). A more illustrative example is shown in Figure 6.22. Nemoto et al. [20] showed evidence of radiation-induced precipitation in various irradiated Mo-Re alloys. Precipitates formed from Mo-4Re alloys after fast neutron irradiation consist of chi and sigma phases.

6.2

Mechanical Properties

Mechanical properties are important to varying degrees in a majority of nuclear reactor components that experience a variety of loading conditions under various temperature and irradiation regimes.

6.2.1

Ceramic Uranium Fuels

Three main ceramic uranium fuels are UO2, UC, and UN (to a smaller extent U3Si and US), i. e. uranium sulfide. The operating experience with UO2 is the greatest even though UN and UC remain the best potential fuels for higher performance in the long term. Improvement in fuel performance and enhanced thermal efficiency require the fuel element temperature to be as high as possible. However, with metallic fuels, two main problems may occur: (a) central fuel melting and (b) excessive irradiation swelling and creep deformation due to irradiation instability at higher temperatures. In this regard, ceramic fuels have certain advan­tages over metallic uranium fuels: (a) higher permissible fuel and plant operating temperatures due to higher melting point, (b) good irradiation stability due to the absence of polymorphic phase transformation, and (c) high corrosion resistance to the environmental attack as a result of its chemical inertness and compatibility with cladding. The basic nuclear properties of competitive ceramic fuels are as follows:

(a) large number of fissile uranium (U235) atoms per unit volume of the fuel in order to avoid necessity for high enrichment, and (b) small neutron absorption cross section of the nonfissile components of the compound for preserving the neutron economy. The following sections discuss various aspects of uranium diox­ide, which is the mainstay of nuclear fuels used in current generation of power reactors. We will briefly discuss UN and UC.

Radiation Effects on Physical Properties

Various physical properties such as thermal conductivity, thermal expansion coefficient, density, elastic constant, and so on are of interest for nuclear

applications. Hence, it is important to understand the irradiation effects on the physical properties. Before we embark on discussing these, we must accept that irradiation can cause various changes in the structure of the materials and thus there may not be a general trend — but the effects will depend on particular situa­tions. So, one needs to be prudent while analyzing these conditions and drawing inferences.

6.3.1 Density

Calculations indicate that vacancy-interstitial pairs should cause substantial changes in the density of the irradiated material as they would increase the volume ~1.5 times theoretically. However, experimental observations show very little or no change in the density (which should decrease due to the generation of Frenkel pairs), except in the radiation swelling regime where volume increase occurs through the creation of voids/bubbles (discussed in Section 6.1.2.2). It is thought that due to the greater mobility of interstitials and their clusters, they would diffuse even at homologous temperatures of 0.15-0.20 and get trapped or annihilated. This implies that we would expect to see little or no change in density of metals/alloys irradiated near or below room temperature. Some exceptions have been seen in very high melting metals such as refractory metals. In such cases, at lower temper­atures, the interstitials are not that mobile, resulting in some significant changes in volume and in turn resulting in decreased density, as observed from lattice parame­ter measurements.

6.3.2