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4007 Aluminum vs. Nickel 600

4007 aluminum belongs to the aluminum alloys classification, while nickel 600 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 4007 aluminum and the bottom bar is nickel 600.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 5.1 to 23
3.4 to 35
Fatigue Strength, MPa 46 to 88
220 to 300
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
75
Shear Strength, MPa 80 to 90
430 to 570
Tensile Strength: Ultimate (UTS), MPa 130 to 160
650 to 990
Tensile Strength: Yield (Proof), MPa 50 to 120
270 to 760

Thermal Properties

Latent Heat of Fusion, J/g 410
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 650
1410
Melting Onset (Solidus), °C 590
1350
Specific Heat Capacity, J/kg-K 890
460
Thermal Conductivity, W/m-K 170
14
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
55
Density, g/cm3 2.8
8.5
Embodied Carbon, kg CO2/kg material 8.1
9.0
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1160
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.4 to 23
31 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 110
190 to 1490
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
23
Strength to Weight: Axial, points 12 to 15
21 to 32
Strength to Weight: Bending, points 20 to 23
20 to 26
Thermal Diffusivity, mm2/s 67
3.6
Thermal Shock Resistance, points 5.5 to 6.7
19 to 29

Alloy Composition

Aluminum (Al), % 94.1 to 97.6
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0.050 to 0.25
14 to 17
Cobalt (Co), % 0 to 0.050
0
Copper (Cu), % 0 to 0.2
0 to 0.5
Iron (Fe), % 0.4 to 1.0
6.0 to 10
Magnesium (Mg), % 0 to 0.2
0
Manganese (Mn), % 0.8 to 1.5
0 to 1.0
Nickel (Ni), % 0.15 to 0.7
72 to 80
Silicon (Si), % 1.0 to 1.7
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0

Comparable Variants