R05252 Alloy vs. C17000 Copper
R05252 alloy belongs to the otherwise unclassified metals classification, while C17000 copper belongs to the copper alloys. There are 18 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is R05252 alloy and the bottom bar is C17000 copper.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
120 |
Elongation at Break, % | 23 | |
1.1 to 31 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 73 | |
45 |
Tensile Strength: Ultimate (UTS), MPa | 310 | |
490 to 1310 |
Tensile Strength: Yield (Proof), MPa | 220 | |
160 to 1140 |
Thermal Properties
Latent Heat of Fusion, J/g | 140 | |
230 |
Specific Heat Capacity, J/kg-K | 140 | |
390 |
Thermal Expansion, µm/m-K | 6.7 | |
17 |
Otherwise Unclassified Properties
Density, g/cm3 | 17 | |
8.8 |
Embodied Water, L/kg | 600 | |
310 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 63 | |
4.2 to 390 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 120 | |
110 to 5420 |
Stiffness to Weight: Axial, points | 6.5 | |
7.6 |
Stiffness to Weight: Bending, points | 12 | |
19 |
Strength to Weight: Axial, points | 5.2 | |
15 to 41 |
Strength to Weight: Bending, points | 6.1 | |
16 to 30 |
Thermal Shock Resistance, points | 17 | |
17 to 45 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.2 |
Beryllium (Be), % | 0 | |
1.6 to 1.8 |
Carbon (C), % | 0 to 0.010 | |
0 |
Copper (Cu), % | 0 | |
96.3 to 98.2 |
Hydrogen (H), % | 0 to 0.0015 | |
0 |
Iron (Fe), % | 0 to 0.010 | |
0 to 0.4 |
Molybdenum (Mo), % | 0 to 0.020 | |
0 |
Nickel (Ni), % | 0 to 0.010 | |
0.2 to 0.6 |
Niobium (Nb), % | 0 to 0.1 | |
0 |
Nitrogen (N), % | 0 to 0.010 | |
0 |
Oxygen (O), % | 0 to 0.015 | |
0 |
Silicon (Si), % | 0 to 0.0050 | |
0 to 0.2 |
Tantalum (Ta), % | 88.8 to 91 | |
0 |
Titanium (Ti), % | 0 to 0.010 | |
0 |
Tungsten (W), % | 9.0 to 11 | |
0 |
Residuals, % | 0 | |
0 to 0.5 |