Grade 23 Titanium vs. SAE-AISI 8740 Steel
Grade 23 titanium belongs to the titanium alloys classification, while SAE-AISI 8740 steel belongs to the iron 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 grade 23 titanium and the bottom bar is SAE-AISI 8740 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
190 |
Elongation at Break, % | 6.7 to 11 | |
11 to 23 |
Fatigue Strength, MPa | 470 to 500 | |
270 to 350 |
Poisson's Ratio | 0.32 | |
0.29 |
Shear Modulus, GPa | 40 | |
73 |
Shear Strength, MPa | 540 to 570 | |
370 to 400 |
Tensile Strength: Ultimate (UTS), MPa | 930 to 940 | |
580 to 670 |
Tensile Strength: Yield (Proof), MPa | 850 to 870 | |
380 to 570 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
250 |
Maximum Temperature: Mechanical, °C | 340 | |
410 |
Melting Completion (Liquidus), °C | 1610 | |
1460 |
Melting Onset (Solidus), °C | 1560 | |
1420 |
Specific Heat Capacity, J/kg-K | 560 | |
470 |
Thermal Conductivity, W/m-K | 7.1 | |
39 |
Thermal Expansion, µm/m-K | 9.4 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
7.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
8.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
2.6 |
Density, g/cm3 | 4.4 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 38 | |
1.5 |
Embodied Energy, MJ/kg | 610 | |
20 |
Embodied Water, L/kg | 200 | |
50 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 61 to 100 | |
71 to 120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 3430 to 3560 | |
390 to 850 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 35 | |
24 |
Strength to Weight: Axial, points | 58 to 59 | |
20 to 24 |
Strength to Weight: Bending, points | 48 | |
20 to 22 |
Thermal Diffusivity, mm2/s | 2.9 | |
10 |
Thermal Shock Resistance, points | 67 to 68 | |
17 to 20 |
Alloy Composition
Aluminum (Al), % | 5.5 to 6.5 | |
0 |
Carbon (C), % | 0 to 0.080 | |
0.38 to 0.43 |
Chromium (Cr), % | 0 | |
0.4 to 0.6 |
Hydrogen (H), % | 0 to 0.013 | |
0 |
Iron (Fe), % | 0 to 0.25 | |
96.5 to 97.7 |
Manganese (Mn), % | 0 | |
0.75 to 1.0 |
Molybdenum (Mo), % | 0 | |
0.2 to 0.3 |
Nickel (Ni), % | 0 | |
0.4 to 0.7 |
Nitrogen (N), % | 0 to 0.030 | |
0 |
Oxygen (O), % | 0 to 0.13 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.035 |
Silicon (Si), % | 0 | |
0.15 to 0.35 |
Sulfur (S), % | 0 | |
0 to 0.040 |
Titanium (Ti), % | 88.1 to 91 | |
0 |
Vanadium (V), % | 3.5 to 4.5 | |
0 |
Residuals, % | 0 to 0.4 | |
0 |