AWS ENiCrCoMo-1 vs. SAE-AISI 1118 Steel
AWS ENiCrCoMo-1 belongs to the nickel alloys classification, while SAE-AISI 1118 steel belongs to the iron alloys. There are 20 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is AWS ENiCrCoMo-1 and the bottom bar is SAE-AISI 1118 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Elongation at Break, % | 28 | |
13 |
Poisson's Ratio | 0.29 | |
0.29 |
Shear Modulus, GPa | 82 | |
73 |
Tensile Strength: Ultimate (UTS), MPa | 710 | |
490 |
Thermal Properties
Latent Heat of Fusion, J/g | 330 | |
250 |
Melting Completion (Liquidus), °C | 1430 | |
1460 |
Melting Onset (Solidus), °C | 1380 | |
1420 |
Specific Heat Capacity, J/kg-K | 440 | |
470 |
Thermal Expansion, µm/m-K | 13 | |
12 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 75 | |
1.9 |
Density, g/cm3 | 8.5 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 11 | |
1.4 |
Embodied Energy, MJ/kg | 140 | |
19 |
Embodied Water, L/kg | 340 | |
47 |
Common Calculations
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
24 |
Strength to Weight: Axial, points | 23 | |
17 |
Strength to Weight: Bending, points | 21 | |
18 |
Thermal Shock Resistance, points | 19 | |
15 |
Alloy Composition
Carbon (C), % | 0.050 to 0.15 | |
0.14 to 0.2 |
Chromium (Cr), % | 21 to 26 | |
0 |
Cobalt (Co), % | 9.0 to 15 | |
0 |
Copper (Cu), % | 0 to 0.5 | |
0 |
Iron (Fe), % | 0 to 5.0 | |
98 to 98.5 |
Manganese (Mn), % | 0.3 to 2.5 | |
1.3 to 1.6 |
Molybdenum (Mo), % | 8.0 to 10 | |
0 |
Nickel (Ni), % | 38.6 to 61.7 | |
0 |
Niobium (Nb), % | 0 to 1.0 | |
0 |
Phosphorus (P), % | 0 to 0.030 | |
0 to 0.040 |
Silicon (Si), % | 0 to 0.75 | |
0 |
Sulfur (S), % | 0 to 0.015 | |
0.080 to 0.13 |
Residuals, % | 0 to 0.5 | |
0 |