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6110A Aluminum vs. N06455 Nickel

6110A aluminum belongs to the aluminum alloys classification, while N06455 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 6110A aluminum and the bottom bar is N06455 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 11 to 18
47
Fatigue Strength, MPa 140 to 210
290
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
82
Shear Strength, MPa 220 to 280
550
Tensile Strength: Ultimate (UTS), MPa 360 to 470
780
Tensile Strength: Yield (Proof), MPa 250 to 430
330

Thermal Properties

Latent Heat of Fusion, J/g 410
320
Maximum Temperature: Mechanical, °C 190
960
Melting Completion (Liquidus), °C 650
1510
Melting Onset (Solidus), °C 600
1450
Specific Heat Capacity, J/kg-K 900
430
Thermal Conductivity, W/m-K 160
10
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
65
Density, g/cm3 2.8
8.8
Embodied Carbon, kg CO2/kg material 8.4
12
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1170
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 47 to 58
300
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 1300
260
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 36 to 47
24
Strength to Weight: Bending, points 41 to 48
21
Thermal Diffusivity, mm2/s 65
2.7
Thermal Shock Resistance, points 16 to 21
24

Alloy Composition

Aluminum (Al), % 94.8 to 98
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0.050 to 0.25
14 to 18
Cobalt (Co), % 0
0 to 2.0
Copper (Cu), % 0.3 to 0.8
0
Iron (Fe), % 0 to 0.5
0 to 3.0
Magnesium (Mg), % 0.7 to 1.1
0
Manganese (Mn), % 0.3 to 0.9
0 to 1.0
Molybdenum (Mo), % 0
14 to 17
Nickel (Ni), % 0
58.1 to 72
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.7 to 1.1
0 to 0.080
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0 to 0.7
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0