SAE-AISI D2 Steel vs. Grade 18 Titanium
SAE-AISI D2 steel belongs to the iron alloys classification, while grade 18 titanium belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is SAE-AISI D2 steel and the bottom bar is grade 18 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 110 |
| Elongation at Break, % | 5.0 to 16 | |
| 11 to 17 |
| Fatigue Strength, MPa | 310 to 860 | |
| 330 to 480 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 75 | |
| 40 |
| Shear Strength, MPa | 460 to 1160 | |
| 420 to 590 |
| Tensile Strength: Ultimate (UTS), MPa | 760 to 2000 | |
| 690 to 980 |
| Tensile Strength: Yield (Proof), MPa | 470 to 1510 | |
| 540 to 810 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 410 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1640 |
| Melting Onset (Solidus), °C | 1390 | |
| 1590 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 550 |
| Thermal Conductivity, W/m-K | 31 | |
| 8.3 |
| Thermal Expansion, µm/m-K | 11 | |
| 9.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 4.3 | |
| 1.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 5.1 | |
| 2.7 |
Otherwise Unclassified Properties
| Density, g/cm3 | 7.7 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 3.4 | |
| 41 |
| Embodied Energy, MJ/kg | 50 | |
| 670 |
| Embodied Water, L/kg | 100 | |
| 270 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 92 to 100 | |
| 87 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 570 to 5940 | |
| 1380 to 3110 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 35 |
| Strength to Weight: Axial, points | 27 to 72 | |
| 43 to 61 |
| Strength to Weight: Bending, points | 24 to 46 | |
| 39 to 49 |
| Thermal Diffusivity, mm2/s | 8.3 | |
| 3.4 |
| Thermal Shock Resistance, points | 25 to 67 | |
| 47 to 67 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 2.5 to 3.5 |
| Carbon (C), % | 1.4 to 1.6 | |
| 0 to 0.080 |
| Chromium (Cr), % | 11 to 13 | |
| 0 |
| Copper (Cu), % | 0 to 0.25 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 81.3 to 86.9 | |
| 0 to 0.25 |
| Manganese (Mn), % | 0 to 0.6 | |
| 0 |
| Molybdenum (Mo), % | 0.7 to 1.2 | |
| 0 |
| Nickel (Ni), % | 0 to 0.3 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.15 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0 to 0.6 | |
| 0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 92.5 to 95.5 |
| Vanadium (V), % | 0 to 1.1 | |
| 2.0 to 3.0 |
| Residuals, % | 0 | |
| 0 to 0.4 |