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Stresses in Cu Thin Films and Ag/Ni Multilayers - Harvard School of ...

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Chapter 2: The Elastic Properties <strong>of</strong> <strong>Cu</strong> Th<strong>in</strong> <strong>Films</strong> 27<br />

Table 2.3: Thermomechanical properties <strong>of</strong> the substrates used for the thermal cycl<strong>in</strong>g<br />

experiments.<br />

Material Ys (GPa) ∗ CTE (10 −6 K −1 ) † Thickness (µm) Ref.<br />

Si(001) 180.5 2.708 395 & 97 [249]<br />

Ge(111) 183.4 5.905 461 [188]<br />

α-Al2O3(0001) 608.4 5.313 257 [86], [249]<br />

fused silica 86.5 0.52 162 [203]<br />

∗ at 25 ◦ C<br />

† at 40 ◦ C<br />

through the (111) pole figure <strong>and</strong> are sufficient to describe fiber textures, although a full<br />

ODF elim<strong>in</strong>ates the peak overlap sometimes present <strong>in</strong> fiber texture plots.<br />

The fiber texture plots were performed on the diffractometer shown <strong>in</strong> Figure 1.5. As<br />

discussed by Wcislak et al. [241], us<strong>in</strong>g a l<strong>in</strong>ear position sensitive detector to f<strong>in</strong>d the<br />

<strong>in</strong>tegrated <strong>in</strong>tensity <strong>of</strong> the peak as a function <strong>of</strong> χ elim<strong>in</strong>ates most <strong>of</strong> the corrections needed<br />

with a po<strong>in</strong>t detector [126, 135], but the th<strong>in</strong> film absorption correction (Appendix B) is still<br />

required. The volume fraction <strong>of</strong> 〈hkl〉-oriented gra<strong>in</strong>s is given by Baker et al. [10]:<br />

where I 111<br />

hkl<br />

fhkl =<br />

� χmax<br />

0<br />

� χmax<br />

0<br />

I 111<br />

hkl s<strong>in</strong> χ dχ<br />

I 111<br />

total<br />

s<strong>in</strong> χ dχ<br />

(2.5)<br />

is the scattered <strong>in</strong>tensity from the 〈hkl〉-oriented gra<strong>in</strong>s <strong>in</strong> the (111) texture plot.<br />

2.3.4 <strong>Cu</strong>rvature Measurements<br />

The wafer curvature apparatus used <strong>in</strong> these experiments was described <strong>in</strong> Chapter<br />

1, <strong>and</strong> the curvatures were converted to stresses us<strong>in</strong>g the Stoney equation (1.16). The<br />

thermomechanical properties <strong>of</strong> the various substrates used are listed <strong>in</strong> Table 2.3.<br />

The films were typically heated <strong>and</strong> cooled at approximately 5 ◦ C/m<strong>in</strong> <strong>in</strong> a form<strong>in</strong>g gas<br />

environment. For the elastic thermal cycles, the heat<strong>in</strong>g <strong>and</strong> cool<strong>in</strong>g rate was varied from

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