Grade 29 Titanium vs. SAE-AISI 4340 Steel
Grade 29 titanium belongs to the titanium alloys classification, while SAE-AISI 4340 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is grade 29 titanium and the bottom bar is SAE-AISI 4340 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 110 | |
190 |
Elongation at Break, % | 6.8 to 11 | |
12 to 22 |
Fatigue Strength, MPa | 460 to 510 | |
330 to 740 |
Poisson's Ratio | 0.32 | |
0.29 |
Shear Modulus, GPa | 40 | |
73 |
Shear Strength, MPa | 550 to 560 | |
430 to 770 |
Tensile Strength: Ultimate (UTS), MPa | 930 to 940 | |
690 to 1280 |
Tensile Strength: Yield (Proof), MPa | 850 to 870 | |
470 to 1150 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
250 |
Maximum Temperature: Mechanical, °C | 340 | |
430 |
Melting Completion (Liquidus), °C | 1610 | |
1460 |
Melting Onset (Solidus), °C | 1560 | |
1420 |
Specific Heat Capacity, J/kg-K | 560 | |
470 |
Thermal Conductivity, W/m-K | 7.3 | |
44 |
Thermal Expansion, µm/m-K | 9.3 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
7.5 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
8.6 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 36 | |
3.5 |
Density, g/cm3 | 4.5 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 39 | |
1.7 |
Embodied Energy, MJ/kg | 640 | |
22 |
Embodied Water, L/kg | 410 | |
53 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 62 to 100 | |
79 to 170 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 3420 to 3540 | |
590 to 3490 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 35 | |
24 |
Strength to Weight: Axial, points | 58 to 59 | |
24 to 45 |
Strength to Weight: Bending, points | 47 to 48 | |
22 to 33 |
Thermal Diffusivity, mm2/s | 2.9 | |
12 |
Thermal Shock Resistance, points | 68 to 69 | |
20 to 38 |
Alloy Composition
Aluminum (Al), % | 5.5 to 6.5 | |
0 |
Carbon (C), % | 0 to 0.080 | |
0.38 to 0.43 |
Chromium (Cr), % | 0 | |
0.7 to 0.9 |
Hydrogen (H), % | 0 to 0.015 | |
0 |
Iron (Fe), % | 0 to 0.25 | |
95.1 to 96.3 |
Manganese (Mn), % | 0 | |
0.6 to 0.8 |
Molybdenum (Mo), % | 0 | |
0.2 to 0.3 |
Nickel (Ni), % | 0 | |
1.7 to 2.0 |
Nitrogen (N), % | 0 to 0.030 | |
0 |
Oxygen (O), % | 0 to 0.13 | |
0 |
Phosphorus (P), % | 0 | |
0 to 0.035 |
Ruthenium (Ru), % | 0.080 to 0.14 | |
0 |
Silicon (Si), % | 0 | |
0.15 to 0.35 |
Sulfur (S), % | 0 | |
0 to 0.040 |
Titanium (Ti), % | 88 to 90.9 | |
0 |
Vanadium (V), % | 3.5 to 4.5 | |
0 |
Residuals, % | 0 to 0.4 | |
0 |