SAE-AISI T1 Steel vs. R58150 Titanium
SAE-AISI T1 steel belongs to the iron alloys classification, while R58150 titanium belongs to the titanium alloys. There are 19 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 SAE-AISI T1 steel and the bottom bar is R58150 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
140 |
Poisson's Ratio | 0.29 | |
0.32 |
Shear Modulus, GPa | 80 | |
52 |
Tensile Strength: Ultimate (UTS), MPa | 770 to 2130 | |
770 |
Thermal Properties
Latent Heat of Fusion, J/g | 240 | |
410 |
Melting Completion (Liquidus), °C | 1810 | |
1760 |
Melting Onset (Solidus), °C | 1750 | |
1700 |
Specific Heat Capacity, J/kg-K | 410 | |
500 |
Thermal Expansion, µm/m-K | 12 | |
8.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 45 | |
48 |
Density, g/cm3 | 9.3 | |
5.4 |
Embodied Carbon, kg CO2/kg material | 8.2 | |
31 |
Embodied Energy, MJ/kg | 130 | |
480 |
Embodied Water, L/kg | 90 | |
150 |
Common Calculations
Stiffness to Weight: Axial, points | 12 | |
14 |
Stiffness to Weight: Bending, points | 21 | |
32 |
Strength to Weight: Axial, points | 23 to 64 | |
40 |
Strength to Weight: Bending, points | 20 to 40 | |
35 |
Thermal Shock Resistance, points | 23 to 64 | |
48 |
Alloy Composition
Carbon (C), % | 0.65 to 0.8 | |
0 to 0.1 |
Chromium (Cr), % | 3.8 to 4.5 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 73.2 to 77.2 | |
0 to 0.1 |
Manganese (Mn), % | 0.1 to 0.4 | |
0 |
Molybdenum (Mo), % | 0 | |
14 to 16 |
Nickel (Ni), % | 0 to 0.3 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.050 |
Oxygen (O), % | 0 | |
0 to 0.2 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Silicon (Si), % | 0.2 to 0.4 | |
0 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Titanium (Ti), % | 0 | |
83.5 to 86 |
Tungsten (W), % | 17.3 to 18.8 | |
0 |
Vanadium (V), % | 0.9 to 1.3 | |
0 |