EN 1.7016 Steel vs. R58150 Titanium
EN 1.7016 steel belongs to the iron alloys classification, while R58150 titanium belongs to the titanium alloys. There are 20 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 EN 1.7016 steel and the bottom bar is R58150 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
140 |
Poisson's Ratio | 0.29 | |
0.32 |
Shear Modulus, GPa | 73 | |
52 |
Tensile Strength: Ultimate (UTS), MPa | 450 to 1390 | |
770 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
410 |
Maximum Temperature: Mechanical, °C | 420 | |
320 |
Melting Completion (Liquidus), °C | 1460 | |
1760 |
Melting Onset (Solidus), °C | 1420 | |
1700 |
Specific Heat Capacity, J/kg-K | 470 | |
500 |
Thermal Expansion, µm/m-K | 13 | |
8.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 2.2 | |
48 |
Density, g/cm3 | 7.8 | |
5.4 |
Embodied Carbon, kg CO2/kg material | 1.4 | |
31 |
Embodied Energy, MJ/kg | 19 | |
480 |
Embodied Water, L/kg | 50 | |
150 |
Common Calculations
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 24 | |
32 |
Strength to Weight: Axial, points | 16 to 49 | |
40 |
Strength to Weight: Bending, points | 17 to 35 | |
35 |
Thermal Shock Resistance, points | 13 to 41 | |
48 |
Alloy Composition
Carbon (C), % | 0.14 to 0.2 | |
0 to 0.1 |
Chromium (Cr), % | 0.7 to 1.0 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 97.3 to 98.6 | |
0 to 0.1 |
Manganese (Mn), % | 0.6 to 0.9 | |
0 |
Molybdenum (Mo), % | 0 | |
14 to 16 |
Nitrogen (N), % | 0 | |
0 to 0.050 |
Oxygen (O), % | 0 | |
0 to 0.2 |
Phosphorus (P), % | 0 to 0.025 | |
0 |
Silicon (Si), % | 0 to 0.3 | |
0 |
Sulfur (S), % | 0 to 0.025 | |
0 |
Titanium (Ti), % | 0 | |
83.5 to 86 |