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5083 Aluminum vs. N06455 Nickel

5083 aluminum belongs to the aluminum alloys classification, while N06455 nickel belongs to the nickel alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 5083 aluminum and the bottom bar is N06455 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 1.1 to 17
47
Fatigue Strength, MPa 93 to 190
290
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
82
Shear Strength, MPa 170 to 220
550
Tensile Strength: Ultimate (UTS), MPa 290 to 390
780
Tensile Strength: Yield (Proof), MPa 110 to 340
330

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 190
960
Melting Completion (Liquidus), °C 640
1510
Melting Onset (Solidus), °C 580
1450
Specific Heat Capacity, J/kg-K 900
430
Thermal Conductivity, W/m-K 120
10
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 96
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
65
Calomel Potential, mV -780
-80
Density, g/cm3 2.7
8.8
Embodied Carbon, kg CO2/kg material 8.9
12
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1170
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.2 to 42
300
Resilience: Unit (Modulus of Resilience), kJ/m3 95 to 860
260
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 29 to 40
24
Strength to Weight: Bending, points 36 to 44
21
Thermal Diffusivity, mm2/s 48
2.7
Thermal Shock Resistance, points 12 to 17
24

Alloy Composition

Aluminum (Al), % 92.4 to 95.6
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 to 0.1
0
Iron (Fe), % 0 to 0.4
0 to 3.0
Magnesium (Mg), % 4.0 to 4.9
0
Manganese (Mn), % 0.4 to 1.0
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 to 0.4
0 to 0.080
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0 to 0.7
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0