SAE-AISI D2 Steel vs. Grade 28 Titanium
SAE-AISI D2 steel belongs to the iron alloys classification, while grade 28 titanium belongs to the titanium alloys. There are 29 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 D2 steel and the bottom bar is grade 28 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
Base Metal Price, % relative | 8.0 | |
36 |
Density, g/cm3 | 7.7 | |
4.5 |
Embodied Carbon, kg CO2/kg material | 3.4 | |
37 |
Embodied Energy, MJ/kg | 50 | |
600 |
Embodied Water, L/kg | 100 | |
370 |
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 | |
1370 to 3100 |
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 66 |
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 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Ruthenium (Ru), % | 0 | |
0.080 to 0.14 |
Silicon (Si), % | 0 to 0.6 | |
0 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Titanium (Ti), % | 0 | |
92.4 to 95.4 |
Vanadium (V), % | 0 to 1.1 | |
2.0 to 3.0 |
Residuals, % | 0 | |
0 to 0.4 |