Grade CW6MC Nickel vs. S13800 Stainless Steel
Grade CW6MC nickel belongs to the nickel alloys classification, while S13800 stainless steel belongs to the iron alloys. They have a modest 26% of their average alloy composition in common, which, by itself, doesn't mean much. There are 29 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is grade CW6MC nickel and the bottom bar is S13800 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
200 |
Elongation at Break, % | 28 | |
11 to 18 |
Fatigue Strength, MPa | 210 | |
410 to 870 |
Poisson's Ratio | 0.29 | |
0.28 |
Shear Modulus, GPa | 79 | |
77 |
Tensile Strength: Ultimate (UTS), MPa | 540 | |
980 to 1730 |
Tensile Strength: Yield (Proof), MPa | 310 | |
660 to 1580 |
Thermal Properties
Latent Heat of Fusion, J/g | 330 | |
280 |
Maximum Temperature: Mechanical, °C | 980 | |
810 |
Melting Completion (Liquidus), °C | 1480 | |
1450 |
Melting Onset (Solidus), °C | 1430 | |
1410 |
Specific Heat Capacity, J/kg-K | 440 | |
470 |
Thermal Conductivity, W/m-K | 11 | |
16 |
Thermal Expansion, µm/m-K | 12 | |
11 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
2.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.4 | |
2.6 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 80 | |
15 |
Density, g/cm3 | 8.6 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 14 | |
3.4 |
Embodied Energy, MJ/kg | 200 | |
46 |
Embodied Water, L/kg | 290 | |
140 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 130 | |
150 to 190 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 240 | |
1090 to 5490 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 23 | |
25 |
Strength to Weight: Axial, points | 18 | |
35 to 61 |
Strength to Weight: Bending, points | 17 | |
28 to 41 |
Thermal Diffusivity, mm2/s | 2.8 | |
4.3 |
Thermal Shock Resistance, points | 15 | |
33 to 58 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.9 to 1.4 |
Carbon (C), % | 0 to 0.060 | |
0 to 0.050 |
Chromium (Cr), % | 20 to 23 | |
12.3 to 13.2 |
Iron (Fe), % | 0 to 5.0 | |
73.6 to 77.3 |
Manganese (Mn), % | 0 to 1.0 | |
0 to 0.2 |
Molybdenum (Mo), % | 8.0 to 10 | |
2.0 to 3.0 |
Nickel (Ni), % | 55.4 to 68.9 | |
7.5 to 8.5 |
Niobium (Nb), % | 3.2 to 4.5 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.010 |
Phosphorus (P), % | 0 to 0.015 | |
0 to 0.010 |
Silicon (Si), % | 0 to 1.0 | |
0 to 0.1 |
Sulfur (S), % | 0 to 0.030 | |
0 to 0.0080 |