Grade 28 Titanium vs. ASTM A372 Grade M Steel
Grade 28 titanium belongs to the titanium alloys classification, while ASTM A372 grade M 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 28 titanium and the bottom bar is ASTM A372 grade M steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
190 |
Elongation at Break, % | 11 to 17 | |
18 to 21 |
Fatigue Strength, MPa | 330 to 480 | |
450 to 520 |
Poisson's Ratio | 0.32 | |
0.29 |
Shear Modulus, GPa | 40 | |
73 |
Shear Strength, MPa | 420 to 590 | |
510 to 570 |
Tensile Strength: Ultimate (UTS), MPa | 690 to 980 | |
810 to 910 |
Tensile Strength: Yield (Proof), MPa | 540 to 810 | |
660 to 770 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
250 |
Maximum Temperature: Mechanical, °C | 330 | |
450 |
Melting Completion (Liquidus), °C | 1640 | |
1460 |
Melting Onset (Solidus), °C | 1590 | |
1420 |
Specific Heat Capacity, J/kg-K | 550 | |
470 |
Thermal Conductivity, W/m-K | 8.3 | |
46 |
Thermal Expansion, µm/m-K | 9.9 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
8.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
9.1 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
5.0 |
Density, g/cm3 | 4.5 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 37 | |
2.0 |
Embodied Energy, MJ/kg | 600 | |
27 |
Embodied Water, L/kg | 370 | |
61 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 87 to 110 | |
160 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1370 to 3100 | |
1140 to 1580 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 35 | |
24 |
Strength to Weight: Axial, points | 43 to 61 | |
29 to 32 |
Strength to Weight: Bending, points | 39 to 49 | |
24 to 27 |
Thermal Diffusivity, mm2/s | 3.4 | |
12 |
Thermal Shock Resistance, points | 47 to 66 | |
24 to 27 |
Alloy Composition
Aluminum (Al), % | 2.5 to 3.5 | |
0 |
Carbon (C), % | 0 to 0.080 | |
0 to 0.23 |
Chromium (Cr), % | 0 | |
1.5 to 2.0 |
Hydrogen (H), % | 0 to 0.015 | |
0 |
Iron (Fe), % | 0 to 0.25 | |
92.5 to 95.1 |
Manganese (Mn), % | 0 | |
0.2 to 0.4 |
Molybdenum (Mo), % | 0 | |
0.4 to 0.6 |
Nickel (Ni), % | 0 | |
2.8 to 3.9 |
Nitrogen (N), % | 0 to 0.030 | |
0 |
Oxygen (O), % | 0 to 0.15 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.015 |
Ruthenium (Ru), % | 0.080 to 0.14 | |
0 |
Silicon (Si), % | 0 | |
0 to 0.3 |
Sulfur (S), % | 0 | |
0 to 0.010 |
Titanium (Ti), % | 92.4 to 95.4 | |
0 |
Vanadium (V), % | 2.0 to 3.0 | |
0 to 0.080 |
Residuals, % | 0 to 0.4 | |
0 |