Nickel 718 vs. Nickel 600
Both nickel 718 and nickel 600 are nickel alloys. They have 77% of their average alloy composition in common. There are 31 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 nickel 718 and the bottom bar is nickel 600.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
190 |
Elongation at Break, % | 12 to 50 | |
3.4 to 35 |
Fatigue Strength, MPa | 460 to 760 | |
220 to 300 |
Poisson's Ratio | 0.29 | |
0.29 |
Shear Modulus, GPa | 75 | |
75 |
Shear Strength, MPa | 660 to 950 | |
430 to 570 |
Tensile Strength: Ultimate (UTS), MPa | 930 to 1530 | |
650 to 990 |
Tensile Strength: Yield (Proof), MPa | 510 to 1330 | |
270 to 760 |
Thermal Properties
Curie Temperature, °C | -110 | |
-120 |
Latent Heat of Fusion, J/g | 310 | |
310 |
Maximum Temperature: Mechanical, °C | 980 | |
1100 |
Melting Completion (Liquidus), °C | 1340 | |
1410 |
Melting Onset (Solidus), °C | 1260 | |
1350 |
Specific Heat Capacity, J/kg-K | 450 | |
460 |
Thermal Conductivity, W/m-K | 11 | |
14 |
Thermal Expansion, µm/m-K | 13 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
1.7 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 1.5 | |
1.8 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 75 | |
55 |
Density, g/cm3 | 8.3 | |
8.5 |
Embodied Carbon, kg CO2/kg material | 13 | |
9.0 |
Embodied Energy, MJ/kg | 190 | |
130 |
Embodied Water, L/kg | 250 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 390 | |
31 to 180 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 660 to 4560 | |
190 to 1490 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 23 | |
23 |
Strength to Weight: Axial, points | 31 to 51 | |
21 to 32 |
Strength to Weight: Bending, points | 25 to 35 | |
20 to 26 |
Thermal Diffusivity, mm2/s | 3.0 | |
3.6 |
Thermal Shock Resistance, points | 27 to 44 | |
19 to 29 |
Alloy Composition
Aluminum (Al), % | 0.2 to 0.8 | |
0 |
Boron (B), % | 0 to 0.0060 | |
0 |
Carbon (C), % | 0 to 0.080 | |
0 to 0.15 |
Chromium (Cr), % | 17 to 21 | |
14 to 17 |
Cobalt (Co), % | 0 to 1.0 | |
0 |
Copper (Cu), % | 0 to 0.3 | |
0 to 0.5 |
Iron (Fe), % | 11.1 to 24.6 | |
6.0 to 10 |
Manganese (Mn), % | 0 to 0.35 | |
0 to 1.0 |
Molybdenum (Mo), % | 2.8 to 3.3 | |
0 |
Nickel (Ni), % | 50 to 55 | |
72 to 80 |
Niobium (Nb), % | 4.8 to 5.5 | |
0 |
Phosphorus (P), % | 0 to 0.015 | |
0 |
Silicon (Si), % | 0 to 0.35 | |
0 to 0.5 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.015 |
Titanium (Ti), % | 0.65 to 1.2 | |
0 |