Grade 5 Titanium vs. AISI 201L Stainless Steel
Grade 5 titanium belongs to the titanium alloys classification, while AISI 201L stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is grade 5 titanium and the bottom bar is AISI 201L stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
200 |
Elongation at Break, % | 8.6 to 11 | |
22 to 46 |
Fatigue Strength, MPa | 530 to 630 | |
270 to 530 |
Poisson's Ratio | 0.32 | |
0.28 |
Shear Modulus, GPa | 40 | |
77 |
Shear Strength, MPa | 600 to 710 | |
520 to 660 |
Tensile Strength: Ultimate (UTS), MPa | 1000 to 1190 | |
740 to 1040 |
Tensile Strength: Yield (Proof), MPa | 910 to 1110 | |
290 to 790 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
280 |
Maximum Temperature: Mechanical, °C | 330 | |
880 |
Melting Completion (Liquidus), °C | 1610 | |
1410 |
Melting Onset (Solidus), °C | 1650 | |
1370 |
Specific Heat Capacity, J/kg-K | 560 | |
480 |
Thermal Conductivity, W/m-K | 6.8 | |
15 |
Thermal Expansion, µm/m-K | 8.9 | |
17 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
2.4 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
2.9 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
12 |
Density, g/cm3 | 4.4 | |
7.7 |
Embodied Carbon, kg CO2/kg material | 38 | |
2.6 |
Embodied Energy, MJ/kg | 610 | |
38 |
Embodied Water, L/kg | 200 | |
140 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 100 to 110 | |
210 to 300 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 3980 to 5880 | |
220 to 1570 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 35 | |
25 |
Strength to Weight: Axial, points | 62 to 75 | |
27 to 37 |
Strength to Weight: Bending, points | 50 to 56 | |
24 to 30 |
Thermal Diffusivity, mm2/s | 2.7 | |
4.0 |
Thermal Shock Resistance, points | 76 to 91 | |
16 to 23 |
Alloy Composition
Aluminum (Al), % | 5.5 to 6.8 | |
0 |
Carbon (C), % | 0 to 0.080 | |
0 to 0.030 |
Chromium (Cr), % | 0 | |
16 to 18 |
Hydrogen (H), % | 0 to 0.015 | |
0 |
Iron (Fe), % | 0 to 0.4 | |
67.9 to 75 |
Manganese (Mn), % | 0 | |
5.5 to 7.5 |
Nickel (Ni), % | 0 | |
3.5 to 5.5 |
Nitrogen (N), % | 0 to 0.050 | |
0 to 0.25 |
Oxygen (O), % | 0 to 0.2 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.045 |
Silicon (Si), % | 0 | |
0 to 0.75 |
Sulfur (S), % | 0 | |
0 to 0.030 |
Titanium (Ti), % | 87.4 to 91 | |
0 |
Vanadium (V), % | 3.5 to 4.5 | |
0 |
Yttrium (Y), % | 0 to 0.0050 | |
0 |
Residuals, % | 0 to 0.4 | |
0 |