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5383 Aluminum vs. Nickel 201

5383 aluminum belongs to the aluminum alloys classification, while nickel 201 belongs to the nickel alloys. There are 30 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 5383 aluminum and the bottom bar is nickel 201.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
180
Elongation at Break, % 6.7 to 15
4.5 to 45
Fatigue Strength, MPa 130 to 200
42 to 210
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 26
70
Shear Strength, MPa 190 to 220
270 to 380
Tensile Strength: Ultimate (UTS), MPa 310 to 370
390 to 660
Tensile Strength: Yield (Proof), MPa 150 to 310
80 to 510

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Mechanical, °C 200
900
Melting Completion (Liquidus), °C 650
1450
Melting Onset (Solidus), °C 540
1440
Specific Heat Capacity, J/kg-K 900
440
Thermal Conductivity, W/m-K 130
78
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
19
Electrical Conductivity: Equal Weight (Specific), % IACS 97
19

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
65
Density, g/cm3 2.7
8.9
Embodied Carbon, kg CO2/kg material 9.0
11
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 1170
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
25 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
17 to 720
Stiffness to Weight: Axial, points 14
11
Stiffness to Weight: Bending, points 50
21
Strength to Weight: Axial, points 32 to 38
12 to 20
Strength to Weight: Bending, points 38 to 42
13 to 19
Thermal Diffusivity, mm2/s 51
20
Thermal Shock Resistance, points 14 to 16
11 to 19

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 0 to 0.25
0 to 0.4
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0 to 0.35
Nickel (Ni), % 0
99 to 100
Silicon (Si), % 0 to 0.25
0 to 0.35
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants