Nickel 601 vs. Nickel 718
Both nickel 601 and nickel 718 are nickel alloys. They have 86% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is nickel 601 and the bottom bar is nickel 718.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
190 |
Elongation at Break, % | 10 to 38 | |
12 to 50 |
Fatigue Strength, MPa | 220 to 380 | |
460 to 760 |
Poisson's Ratio | 0.28 | |
0.29 |
Shear Modulus, GPa | 76 | |
75 |
Shear Strength, MPa | 440 to 530 | |
660 to 950 |
Tensile Strength: Ultimate (UTS), MPa | 660 to 890 | |
930 to 1530 |
Tensile Strength: Yield (Proof), MPa | 290 to 800 | |
510 to 1330 |
Thermal Properties
Curie Temperature, °C | -200 | |
-110 |
Latent Heat of Fusion, J/g | 320 | |
310 |
Maximum Temperature: Mechanical, °C | 1100 | |
980 |
Melting Completion (Liquidus), °C | 1410 | |
1340 |
Melting Onset (Solidus), °C | 1360 | |
1260 |
Specific Heat Capacity, J/kg-K | 470 | |
450 |
Thermal Conductivity, W/m-K | 11 | |
11 |
Thermal Expansion, µm/m-K | 14 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.5 | |
1.4 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.6 | |
1.5 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 49 | |
75 |
Density, g/cm3 | 8.3 | |
8.3 |
Embodied Carbon, kg CO2/kg material | 8.0 | |
13 |
Embodied Energy, MJ/kg | 110 | |
190 |
Embodied Water, L/kg | 280 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 86 to 200 | |
140 to 390 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 210 to 1630 | |
660 to 4560 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
23 |
Strength to Weight: Axial, points | 22 to 30 | |
31 to 51 |
Strength to Weight: Bending, points | 20 to 25 | |
25 to 35 |
Thermal Diffusivity, mm2/s | 2.8 | |
3.0 |
Thermal Shock Resistance, points | 17 to 23 | |
27 to 44 |
Alloy Composition
Aluminum (Al), % | 1.0 to 1.7 | |
0.2 to 0.8 |
Boron (B), % | 0 | |
0 to 0.0060 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.080 |
Chromium (Cr), % | 21 to 25 | |
17 to 21 |
Cobalt (Co), % | 0 | |
0 to 1.0 |
Copper (Cu), % | 0 to 1.0 | |
0 to 0.3 |
Iron (Fe), % | 7.7 to 20 | |
11.1 to 24.6 |
Manganese (Mn), % | 0 to 1.0 | |
0 to 0.35 |
Molybdenum (Mo), % | 0 | |
2.8 to 3.3 |
Nickel (Ni), % | 58 to 63 | |
50 to 55 |
Niobium (Nb), % | 0 | |
4.8 to 5.5 |
Phosphorus (P), % | 0 | |
0 to 0.015 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.35 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.015 |
Titanium (Ti), % | 0 | |
0.65 to 1.2 |