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Table 1 Material data for the copper alloy CuCr1Zr

From: Stress evolution in thermal barrier coatings for rocket engine applications

Thermal Conductivity / W/m K (Kupferinstitut 2005) Temp / K  
320 293.14  
315 373.14  
324 473.14  
333 573.14  
336 673.14  
Coefficient of thermal expansion (Dies 1967; Kupferinstitut 2005) / K −1 Temp / K  
16.3×10−6 373.14  
17.0×10−6 473.14  
17.6×10−6 573.14  
18.3×10−6 873.14  
19.0×10−6 973.14  
19.8×10−6 1173.14  
20.9×10−6 1356.14  
Specific Heat (Kupferinstitut 2005) / J/kg K Temp  
370 293.14  
450 373.14  
480 473.14  
500 573.14  
500 673.14  
Density (Kupferinstitut 2005) / kg/m3   
8.91×103   
Young’s modulus (Kupferinstitut 2005) / GPa Poisson’s ratio (Fassin 2015) Temp / K
120 0.30 293.14
87 0.31 873.14
Yield stress (Baukloh et al. 1976; Kupferinstitut 2005; Zinkle and Fabritsiev 1994) / MPa Temp / K  
380 293  
250 573  
200 723  
150 873  
70 973