EN 1.6570 Steel vs. ASTM B817 Type I
EN 1.6570 steel belongs to the iron alloys classification, while ASTM B817 type I belongs to the titanium alloys. There are 29 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 EN 1.6570 steel and the bottom bar is ASTM B817 type I.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
100 |
Elongation at Break, % | 11 to 17 | |
4.0 to 13 |
Fatigue Strength, MPa | 500 to 660 | |
360 to 520 |
Poisson's Ratio | 0.29 | |
0.32 |
Shear Modulus, GPa | 73 | |
40 |
Tensile Strength: Ultimate (UTS), MPa | 910 to 1130 | |
770 to 960 |
Tensile Strength: Yield (Proof), MPa | 760 to 1060 | |
700 to 860 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
410 |
Maximum Temperature: Mechanical, °C | 440 | |
340 |
Melting Completion (Liquidus), °C | 1460 | |
1600 |
Melting Onset (Solidus), °C | 1420 | |
1550 |
Specific Heat Capacity, J/kg-K | 470 | |
560 |
Thermal Conductivity, W/m-K | 40 | |
7.1 |
Thermal Expansion, µm/m-K | 13 | |
9.6 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.7 | |
1.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 8.8 | |
2.0 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 3.9 | |
36 |
Density, g/cm3 | 7.9 | |
4.4 |
Embodied Carbon, kg CO2/kg material | 1.7 | |
38 |
Embodied Energy, MJ/kg | 23 | |
610 |
Embodied Water, L/kg | 56 | |
200 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 120 to 140 | |
30 to 120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1520 to 3010 | |
2310 to 3540 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
35 |
Strength to Weight: Axial, points | 32 to 40 | |
48 to 60 |
Strength to Weight: Bending, points | 27 to 31 | |
42 to 49 |
Thermal Diffusivity, mm2/s | 11 | |
2.9 |
Thermal Shock Resistance, points | 27 to 33 | |
54 to 68 |
Alloy Composition
Aluminum (Al), % | 0 | |
5.5 to 6.8 |
Carbon (C), % | 0.28 to 0.35 | |
0 to 0.1 |
Chlorine (Cl), % | 0 | |
0 to 0.2 |
Chromium (Cr), % | 1.0 to 1.4 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 94 to 96.2 | |
0 to 0.4 |
Manganese (Mn), % | 0.6 to 1.0 | |
0 |
Molybdenum (Mo), % | 0.3 to 0.5 | |
0 |
Nickel (Ni), % | 1.6 to 2.1 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.040 |
Oxygen (O), % | 0 | |
0 to 0.3 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 0.6 | |
0 to 0.1 |
Sodium (Na), % | 0 | |
0 to 0.2 |
Sulfur (S), % | 0 to 0.015 | |
0 |
Titanium (Ti), % | 0 | |
87 to 91 |
Vanadium (V), % | 0 | |
3.5 to 4.5 |
Residuals, % | 0 | |
0 to 0.4 |