EN 1.5535 Steel vs. Grade 35 Titanium
EN 1.5535 steel belongs to the iron alloys classification, while grade 35 titanium belongs to the titanium alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is EN 1.5535 steel and the bottom bar is grade 35 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
110 |
Elongation at Break, % | 11 to 22 | |
5.6 |
Fatigue Strength, MPa | 210 to 320 | |
330 |
Poisson's Ratio | 0.29 | |
0.32 |
Reduction in Area, % | 62 to 72 | |
23 |
Shear Modulus, GPa | 73 | |
41 |
Shear Strength, MPa | 320 to 370 | |
580 |
Tensile Strength: Ultimate (UTS), MPa | 450 to 1490 | |
1000 |
Tensile Strength: Yield (Proof), MPa | 300 to 500 | |
630 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
420 |
Maximum Temperature: Mechanical, °C | 400 | |
320 |
Melting Completion (Liquidus), °C | 1460 | |
1630 |
Melting Onset (Solidus), °C | 1420 | |
1580 |
Specific Heat Capacity, J/kg-K | 470 | |
550 |
Thermal Conductivity, W/m-K | 50 | |
7.4 |
Thermal Expansion, µm/m-K | 13 | |
9.3 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.2 | |
1.1 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 8.2 | |
2.2 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 1.9 | |
37 |
Density, g/cm3 | 7.8 | |
4.6 |
Embodied Carbon, kg CO2/kg material | 1.4 | |
33 |
Embodied Energy, MJ/kg | 19 | |
530 |
Embodied Water, L/kg | 48 | |
170 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 45 to 250 | |
49 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 240 to 680 | |
1830 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
35 |
Strength to Weight: Axial, points | 16 to 53 | |
61 |
Strength to Weight: Bending, points | 17 to 37 | |
49 |
Thermal Diffusivity, mm2/s | 13 | |
3.0 |
Thermal Shock Resistance, points | 13 to 44 | |
70 |
Alloy Composition
Aluminum (Al), % | 0 | |
4.0 to 5.0 |
Boron (B), % | 0.00080 to 0.0050 | |
0 |
Carbon (C), % | 0.2 to 0.25 | |
0 to 0.080 |
Chromium (Cr), % | 0 to 0.3 | |
0 |
Copper (Cu), % | 0 to 0.25 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 97.6 to 98.9 | |
0.2 to 0.8 |
Manganese (Mn), % | 0.9 to 1.2 | |
0 |
Molybdenum (Mo), % | 0 | |
1.5 to 2.5 |
Nitrogen (N), % | 0 | |
0 to 0.050 |
Oxygen (O), % | 0 | |
0 to 0.25 |
Phosphorus (P), % | 0 to 0.025 | |
0 |
Silicon (Si), % | 0 to 0.3 | |
0.2 to 0.4 |
Sulfur (S), % | 0 to 0.025 | |
0 |
Titanium (Ti), % | 0 | |
88.4 to 93 |
Vanadium (V), % | 0 | |
1.1 to 2.1 |
Residuals, % | 0 | |
0 to 0.4 |