ASTM A182 Grade F1 vs. R30556 Alloy
Both ASTM A182 grade F1 and R30556 alloy are iron alloys. Both are furnished in the annealed condition. They have a modest 31% of their average alloy composition in common, which, by itself, doesn't mean much. There are 30 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 ASTM A182 grade F1 and the bottom bar is R30556 alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
210 |
Elongation at Break, % | 22 | |
45 |
Fatigue Strength, MPa | 220 | |
320 |
Poisson's Ratio | 0.29 | |
0.28 |
Shear Modulus, GPa | 73 | |
81 |
Shear Strength, MPa | 340 | |
550 |
Tensile Strength: Ultimate (UTS), MPa | 540 | |
780 |
Tensile Strength: Yield (Proof), MPa | 310 | |
350 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
300 |
Maximum Temperature: Mechanical, °C | 410 | |
1100 |
Melting Completion (Liquidus), °C | 1470 | |
1420 |
Melting Onset (Solidus), °C | 1420 | |
1330 |
Specific Heat Capacity, J/kg-K | 470 | |
450 |
Thermal Conductivity, W/m-K | 50 | |
11 |
Thermal Expansion, µm/m-K | 13 | |
15 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.1 | |
1.8 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 8.2 | |
1.9 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 2.4 | |
70 |
Density, g/cm3 | 7.9 | |
8.4 |
Embodied Carbon, kg CO2/kg material | 1.5 | |
8.7 |
Embodied Energy, MJ/kg | 20 | |
130 |
Embodied Water, L/kg | 48 | |
300 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 100 | |
290 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 260 | |
290 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 24 | |
23 |
Strength to Weight: Axial, points | 19 | |
26 |
Strength to Weight: Bending, points | 19 | |
22 |
Thermal Diffusivity, mm2/s | 13 | |
2.9 |
Thermal Shock Resistance, points | 16 | |
18 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.1 to 0.5 |
Boron (B), % | 0 | |
0 to 0.020 |
Carbon (C), % | 0 to 0.28 | |
0.050 to 0.15 |
Chromium (Cr), % | 0 | |
21 to 23 |
Cobalt (Co), % | 0 | |
16 to 21 |
Iron (Fe), % | 97.7 to 98.8 | |
20.4 to 38.2 |
Lanthanum (La), % | 0 | |
0.0050 to 0.1 |
Manganese (Mn), % | 0.6 to 0.9 | |
0.5 to 2.0 |
Molybdenum (Mo), % | 0.44 to 0.65 | |
2.5 to 4.0 |
Nickel (Ni), % | 0 | |
19 to 22.5 |
Niobium (Nb), % | 0 | |
0 to 0.3 |
Nitrogen (N), % | 0 | |
0.1 to 0.3 |
Phosphorus (P), % | 0 to 0.045 | |
0 to 0.040 |
Silicon (Si), % | 0.15 to 0.35 | |
0.2 to 0.8 |
Sulfur (S), % | 0 to 0.045 | |
0 to 0.015 |
Tantalum (Ta), % | 0 | |
0.3 to 1.3 |
Tungsten (W), % | 0 | |
2.0 to 3.5 |
Zinc (Zn), % | 0 | |
0.0010 to 0.1 |