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5454 Aluminum vs. Nickel 601

5454 aluminum belongs to the aluminum alloys classification, while nickel 601 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 5454 aluminum and the bottom bar is nickel 601.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 2.3 to 18
10 to 38
Fatigue Strength, MPa 83 to 160
220 to 380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 140 to 200
440 to 530
Tensile Strength: Ultimate (UTS), MPa 230 to 350
660 to 890
Tensile Strength: Yield (Proof), MPa 97 to 290
290 to 800

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 190
1100
Melting Completion (Liquidus), °C 650
1410
Melting Onset (Solidus), °C 600
1360
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
11
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 110
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
49
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.6
8.0
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1180
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.3 to 34
86 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 590
210 to 1630
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 23 to 36
22 to 30
Strength to Weight: Bending, points 30 to 41
20 to 25
Thermal Diffusivity, mm2/s 55
2.8
Thermal Shock Resistance, points 10 to 16
17 to 23

Alloy Composition

Aluminum (Al), % 94.5 to 97.1
1.0 to 1.7
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.050 to 0.2
21 to 25
Copper (Cu), % 0 to 0.1
0 to 1.0
Iron (Fe), % 0 to 0.4
7.7 to 20
Magnesium (Mg), % 2.4 to 3.0
0
Manganese (Mn), % 0.5 to 1.0
0 to 1.0
Nickel (Ni), % 0
58 to 63
Silicon (Si), % 0 to 0.25
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants