Grade 18 Titanium vs. 60Cr-40Ni Alloy
Grade 18 titanium belongs to the titanium alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 18 material properties with values for both materials. Properties with values for just one material (13, in this case) are not shown.
For each property being compared, the top bar is grade 18 titanium and the bottom bar is 60Cr-40Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
220 |
Poisson's Ratio | 0.32 | |
0.25 |
Shear Modulus, GPa | 40 | |
87 |
Tensile Strength: Ultimate (UTS), MPa | 690 to 980 | |
870 |
Tensile Strength: Yield (Proof), MPa | 540 to 810 | |
660 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
370 |
Specific Heat Capacity, J/kg-K | 550 | |
490 |
Thermal Expansion, µm/m-K | 9.9 | |
16 |
Otherwise Unclassified Properties
Density, g/cm3 | 4.5 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 41 | |
7.4 |
Embodied Energy, MJ/kg | 670 | |
110 |
Embodied Water, L/kg | 270 | |
380 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1380 to 3110 | |
1000 |
Stiffness to Weight: Axial, points | 13 | |
16 |
Stiffness to Weight: Bending, points | 35 | |
26 |
Strength to Weight: Axial, points | 43 to 61 | |
31 |
Strength to Weight: Bending, points | 39 to 49 | |
26 |
Thermal Shock Resistance, points | 47 to 67 | |
18 |
Alloy Composition
Aluminum (Al), % | 2.5 to 3.5 | |
0 to 0.25 |
Carbon (C), % | 0 to 0.080 | |
0 to 0.1 |
Chromium (Cr), % | 0 | |
58 to 62 |
Hydrogen (H), % | 0 to 0.015 | |
0 |
Iron (Fe), % | 0 to 0.25 | |
0 to 1.0 |
Manganese (Mn), % | 0 | |
0 to 0.3 |
Nickel (Ni), % | 0 | |
34.5 to 42 |
Nitrogen (N), % | 0 to 0.030 | |
0 to 0.3 |
Oxygen (O), % | 0 to 0.15 | |
0 |
Palladium (Pd), % | 0.040 to 0.080 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.020 |
Silicon (Si), % | 0 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.020 |
Titanium (Ti), % | 92.5 to 95.5 | |
0 to 0.5 |
Vanadium (V), % | 2.0 to 3.0 | |
0 |
Residuals, % | 0 to 0.4 | |
0 |