SAE-AISI 6150 Steel vs. Grade 23 Titanium
SAE-AISI 6150 steel belongs to the iron alloys classification, while grade 23 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is SAE-AISI 6150 steel and the bottom bar is grade 23 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
110 |
Elongation at Break, % | 15 to 23 | |
6.7 to 11 |
Fatigue Strength, MPa | 300 to 750 | |
470 to 500 |
Poisson's Ratio | 0.29 | |
0.32 |
Shear Modulus, GPa | 73 | |
40 |
Shear Strength, MPa | 400 to 730 | |
540 to 570 |
Tensile Strength: Ultimate (UTS), MPa | 630 to 1200 | |
930 to 940 |
Tensile Strength: Yield (Proof), MPa | 420 to 1160 | |
850 to 870 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
410 |
Maximum Temperature: Mechanical, °C | 420 | |
340 |
Melting Completion (Liquidus), °C | 1460 | |
1610 |
Melting Onset (Solidus), °C | 1410 | |
1560 |
Specific Heat Capacity, J/kg-K | 470 | |
560 |
Thermal Conductivity, W/m-K | 46 | |
7.1 |
Thermal Expansion, µm/m-K | 12 to 13 | |
9.4 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.3 | |
1.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 8.4 | |
2.0 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 2.3 | |
36 |
Density, g/cm3 | 7.8 | |
4.4 |
Embodied Carbon, kg CO2/kg material | 2.0 | |
38 |
Embodied Energy, MJ/kg | 28 | |
610 |
Embodied Water, L/kg | 51 | |
200 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 130 to 180 | |
61 to 100 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 3590 | |
3430 to 3560 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
35 |
Strength to Weight: Axial, points | 22 to 43 | |
58 to 59 |
Strength to Weight: Bending, points | 21 to 32 | |
48 |
Thermal Diffusivity, mm2/s | 13 | |
2.9 |
Thermal Shock Resistance, points | 20 to 38 | |
67 to 68 |
Alloy Composition
Aluminum (Al), % | 0 | |
5.5 to 6.5 |
Carbon (C), % | 0.48 to 0.53 | |
0 to 0.080 |
Chromium (Cr), % | 0.8 to 1.1 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.013 |
Iron (Fe), % | 96.7 to 97.7 | |
0 to 0.25 |
Manganese (Mn), % | 0.7 to 0.9 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.030 |
Oxygen (O), % | 0 | |
0 to 0.13 |
Phosphorus (P), % | 0 to 0.035 | |
0 |
Silicon (Si), % | 0.15 to 0.35 | |
0 |
Sulfur (S), % | 0 to 0.040 | |
0 |
Titanium (Ti), % | 0 | |
88.1 to 91 |
Vanadium (V), % | 0.15 to 0.3 | |
3.5 to 4.5 |
Residuals, % | 0 | |
0 to 0.4 |