60Cr-40Ni Alloy vs. Grade 28 Titanium
60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while grade 28 titanium belongs to the titanium alloys. There are 19 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.
For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is grade 28 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 220 | |
110 |
Poisson's Ratio | 0.25 | |
0.32 |
Shear Modulus, GPa | 87 | |
40 |
Tensile Strength: Ultimate (UTS), MPa | 870 | |
690 to 980 |
Tensile Strength: Yield (Proof), MPa | 660 | |
540 to 810 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
410 |
Specific Heat Capacity, J/kg-K | 490 | |
550 |
Thermal Expansion, µm/m-K | 16 | |
9.9 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 49 | |
36 |
Density, g/cm3 | 7.8 | |
4.5 |
Embodied Carbon, kg CO2/kg material | 7.4 | |
37 |
Embodied Energy, MJ/kg | 110 | |
600 |
Embodied Water, L/kg | 380 | |
370 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1000 | |
1370 to 3100 |
Stiffness to Weight: Axial, points | 16 | |
13 |
Stiffness to Weight: Bending, points | 26 | |
35 |
Strength to Weight: Axial, points | 31 | |
43 to 61 |
Strength to Weight: Bending, points | 26 | |
39 to 49 |
Thermal Shock Resistance, points | 18 | |
47 to 66 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
2.5 to 3.5 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.080 |
Chromium (Cr), % | 58 to 62 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 0 to 1.0 | |
0 to 0.25 |
Manganese (Mn), % | 0 to 0.3 | |
0 |
Nickel (Ni), % | 34.5 to 42 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 to 0.030 |
Oxygen (O), % | 0 | |
0 to 0.15 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Ruthenium (Ru), % | 0 | |
0.080 to 0.14 |
Silicon (Si), % | 0 to 1.0 | |
0 |
Sulfur (S), % | 0 to 0.020 | |
0 |
Titanium (Ti), % | 0 to 0.5 | |
92.4 to 95.4 |
Vanadium (V), % | 0 | |
2.0 to 3.0 |
Residuals, % | 0 | |
0 to 0.4 |