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5182 Aluminum vs. Nickel 200

5182 aluminum belongs to the aluminum alloys classification, while nickel 200 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 5182 aluminum and the bottom bar is nickel 200.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
180
Elongation at Break, % 1.1 to 12
23 to 44
Fatigue Strength, MPa 100 to 130
120 to 350
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 25
70
Shear Strength, MPa 170 to 240
300 to 340
Tensile Strength: Ultimate (UTS), MPa 280 to 420
420 to 540
Tensile Strength: Yield (Proof), MPa 130 to 360
120 to 370

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Mechanical, °C 180
900
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 590
1440
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 130
69
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
18
Electrical Conductivity: Equal Weight (Specific), % IACS 94
18

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
65
Density, g/cm3 2.7
8.9
Embodied Carbon, kg CO2/kg material 8.9
11
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.6 to 49
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 950
42 to 370
Stiffness to Weight: Axial, points 14
11
Stiffness to Weight: Bending, points 51
21
Strength to Weight: Axial, points 29 to 44
13 to 17
Strength to Weight: Bending, points 36 to 47
14 to 17
Thermal Diffusivity, mm2/s 53
17
Thermal Shock Resistance, points 12 to 19
13 to 16

Alloy Composition

Aluminum (Al), % 93.2 to 95.8
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.15
0 to 0.25
Iron (Fe), % 0 to 0.35
0 to 0.4
Magnesium (Mg), % 4.0 to 5.0
0
Manganese (Mn), % 0.2 to 0.5
0 to 0.35
Nickel (Ni), % 0
99 to 100
Silicon (Si), % 0 to 0.2
0 to 0.35
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants