Grade 28 Titanium vs. S21904 Stainless Steel
Grade 28 titanium belongs to the titanium alloys classification, while S21904 stainless steel belongs to the iron alloys. There are 30 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 grade 28 titanium and the bottom bar is S21904 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
200 |
Elongation at Break, % | 11 to 17 | |
17 to 51 |
Fatigue Strength, MPa | 330 to 480 | |
380 to 550 |
Poisson's Ratio | 0.32 | |
0.28 |
Shear Modulus, GPa | 40 | |
78 |
Shear Strength, MPa | 420 to 590 | |
510 to 620 |
Tensile Strength: Ultimate (UTS), MPa | 690 to 980 | |
700 to 1000 |
Tensile Strength: Yield (Proof), MPa | 540 to 810 | |
390 to 910 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
290 |
Maximum Temperature: Mechanical, °C | 330 | |
980 |
Melting Completion (Liquidus), °C | 1640 | |
1400 |
Melting Onset (Solidus), °C | 1590 | |
1350 |
Specific Heat Capacity, J/kg-K | 550 | |
480 |
Thermal Conductivity, W/m-K | 8.3 | |
14 |
Thermal Expansion, µm/m-K | 9.9 | |
17 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
2.5 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
2.9 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
15 |
Density, g/cm3 | 4.5 | |
7.7 |
Embodied Carbon, kg CO2/kg material | 37 | |
3.0 |
Embodied Energy, MJ/kg | 600 | |
43 |
Embodied Water, L/kg | 370 | |
160 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 87 to 110 | |
160 to 310 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1370 to 3100 | |
380 to 2070 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 35 | |
25 |
Strength to Weight: Axial, points | 43 to 61 | |
25 to 36 |
Strength to Weight: Bending, points | 39 to 49 | |
23 to 29 |
Thermal Diffusivity, mm2/s | 3.4 | |
3.8 |
Thermal Shock Resistance, points | 47 to 66 | |
15 to 21 |
Alloy Composition
Aluminum (Al), % | 2.5 to 3.5 | |
0 |
Carbon (C), % | 0 to 0.080 | |
0 to 0.040 |
Chromium (Cr), % | 0 | |
19 to 21.5 |
Hydrogen (H), % | 0 to 0.015 | |
0 |
Iron (Fe), % | 0 to 0.25 | |
59.5 to 67.4 |
Manganese (Mn), % | 0 | |
8.0 to 10 |
Nickel (Ni), % | 0 | |
5.5 to 7.5 |
Nitrogen (N), % | 0 to 0.030 | |
0.15 to 0.4 |
Oxygen (O), % | 0 to 0.15 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.045 |
Ruthenium (Ru), % | 0.080 to 0.14 | |
0 |
Silicon (Si), % | 0 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.030 |
Titanium (Ti), % | 92.4 to 95.4 | |
0 |
Vanadium (V), % | 2.0 to 3.0 | |
0 |
Residuals, % | 0 to 0.4 | |
0 |