R30556 Alloy vs. EN 1.6580 Steel
Both R30556 alloy and EN 1.6580 steel are iron alloys. They have a modest 34% of their average alloy composition in common, which, by itself, doesn't mean much. There are 31 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 R30556 alloy and the bottom bar is EN 1.6580 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Elongation at Break, % | 45 | |
11 to 19 |
Fatigue Strength, MPa | 320 | |
310 to 610 |
Poisson's Ratio | 0.28 | |
0.29 |
Shear Modulus, GPa | 81 | |
73 |
Shear Strength, MPa | 550 | |
450 to 700 |
Tensile Strength: Ultimate (UTS), MPa | 780 | |
720 to 1170 |
Tensile Strength: Yield (Proof), MPa | 350 | |
460 to 990 |
Thermal Properties
Latent Heat of Fusion, J/g | 300 | |
250 |
Maximum Temperature: Mechanical, °C | 1100 | |
450 |
Melting Completion (Liquidus), °C | 1420 | |
1460 |
Melting Onset (Solidus), °C | 1330 | |
1420 |
Specific Heat Capacity, J/kg-K | 450 | |
470 |
Thermal Conductivity, W/m-K | 11 | |
40 |
Thermal Expansion, µm/m-K | 15 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.8 | |
7.8 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.9 | |
8.9 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 70 | |
4.3 |
Density, g/cm3 | 8.4 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 8.7 | |
1.8 |
Embodied Energy, MJ/kg | 130 | |
23 |
Embodied Water, L/kg | 300 | |
59 |
Common Calculations
PREN (Pitting Resistance) | 40 | |
3.3 |
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 290 | |
120 to 130 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 290 | |
560 to 2590 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
24 |
Strength to Weight: Axial, points | 26 | |
26 to 41 |
Strength to Weight: Bending, points | 22 | |
23 to 31 |
Thermal Diffusivity, mm2/s | 2.9 | |
11 |
Thermal Shock Resistance, points | 18 | |
21 to 34 |
Alloy Composition
Aluminum (Al), % | 0.1 to 0.5 | |
0 |
Boron (B), % | 0 to 0.020 | |
0 |
Carbon (C), % | 0.050 to 0.15 | |
0.26 to 0.34 |
Chromium (Cr), % | 21 to 23 | |
1.8 to 2.2 |
Cobalt (Co), % | 16 to 21 | |
0 |
Iron (Fe), % | 20.4 to 38.2 | |
93.7 to 95.5 |
Lanthanum (La), % | 0.0050 to 0.1 | |
0 |
Manganese (Mn), % | 0.5 to 2.0 | |
0.3 to 0.6 |
Molybdenum (Mo), % | 2.5 to 4.0 | |
0.3 to 0.5 |
Nickel (Ni), % | 19 to 22.5 | |
1.8 to 2.2 |
Niobium (Nb), % | 0 to 0.3 | |
0 |
Nitrogen (N), % | 0.1 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.040 | |
0 to 0.035 |
Silicon (Si), % | 0.2 to 0.8 | |
0 to 0.4 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.035 |
Tantalum (Ta), % | 0.3 to 1.3 | |
0 |
Tungsten (W), % | 2.0 to 3.5 | |
0 |
Zinc (Zn), % | 0.0010 to 0.1 | |
0 |