MakeItFrom.com
Menu (ESC)

5050 Aluminum vs. N06002 Nickel

5050 aluminum belongs to the aluminum alloys classification, while N06002 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 5050 aluminum and the bottom bar is N06002 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 1.7 to 22
41
Fatigue Strength, MPa 45 to 100
250
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 91 to 140
520
Tensile Strength: Ultimate (UTS), MPa 140 to 250
760
Tensile Strength: Yield (Proof), MPa 50 to 210
310

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 180
990
Melting Completion (Liquidus), °C 650
1360
Melting Onset (Solidus), °C 630
1260
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 190
9.9
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 50
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 170
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
55
Density, g/cm3 2.7
8.5
Embodied Carbon, kg CO2/kg material 8.4
9.3
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1190
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.1 to 24
250
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 330
230
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 15 to 26
25
Strength to Weight: Bending, points 22 to 33
22
Thermal Diffusivity, mm2/s 79
2.6
Thermal Shock Resistance, points 6.3 to 11
19

Alloy Composition

Aluminum (Al), % 96.3 to 98.9
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.1
20.5 to 23
Cobalt (Co), % 0
0.5 to 2.5
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.7
17 to 20
Magnesium (Mg), % 1.1 to 1.8
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
42.3 to 54
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tungsten (W), % 0
0.2 to 1.0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0