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Nickel 718 vs. 6005A Aluminum

Nickel 718 belongs to the nickel alloys classification, while 6005A aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is nickel 718 and the bottom bar is 6005A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 12 to 50
8.6 to 17
Fatigue Strength, MPa 460 to 760
55 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 660 to 950
120 to 180
Tensile Strength: Ultimate (UTS), MPa 930 to 1530
190 to 300
Tensile Strength: Yield (Proof), MPa 510 to 1330
100 to 270

Thermal Properties

Latent Heat of Fusion, J/g 310
410
Maximum Temperature: Mechanical, °C 980
170
Melting Completion (Liquidus), °C 1340
650
Melting Onset (Solidus), °C 1260
600
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 11
180 to 190
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
47 to 50
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
150 to 170

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 8.3
2.7
Embodied Carbon, kg CO2/kg material 13
8.3
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 250
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 390
24 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 660 to 4560
76 to 530
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 31 to 51
20 to 30
Strength to Weight: Bending, points 25 to 35
27 to 36
Thermal Diffusivity, mm2/s 3.0
72 to 79
Thermal Shock Resistance, points 27 to 44
8.6 to 13

Alloy Composition

Aluminum (Al), % 0.2 to 0.8
96.5 to 99.1
Boron (B), % 0 to 0.0060
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 17 to 21
0 to 0.3
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.3
0 to 0.3
Iron (Fe), % 11.1 to 24.6
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.7
Manganese (Mn), % 0 to 0.35
0 to 0.5
Molybdenum (Mo), % 2.8 to 3.3
0
Nickel (Ni), % 50 to 55
0
Niobium (Nb), % 4.8 to 5.5
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.35
0.5 to 0.9
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.65 to 1.2
0 to 0.1
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15