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N06002 Nickel vs. 7005 Aluminum

N06002 nickel belongs to the nickel alloys classification, while 7005 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 N06002 nickel and the bottom bar is 7005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
70
Elongation at Break, % 41
10 to 20
Fatigue Strength, MPa 250
100 to 190
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 81
26
Shear Strength, MPa 520
120 to 230
Tensile Strength: Ultimate (UTS), MPa 760
200 to 400
Tensile Strength: Yield (Proof), MPa 310
95 to 350

Thermal Properties

Latent Heat of Fusion, J/g 320
380
Maximum Temperature: Mechanical, °C 990
200
Melting Completion (Liquidus), °C 1360
640
Melting Onset (Solidus), °C 1260
610
Specific Heat Capacity, J/kg-K 450
880
Thermal Conductivity, W/m-K 9.9
140 to 170
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
35 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
110 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 55
9.5
Density, g/cm3 8.5
2.9
Embodied Carbon, kg CO2/kg material 9.3
8.3
Embodied Energy, MJ/kg 130
150
Embodied Water, L/kg 270
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 250
32 to 57
Resilience: Unit (Modulus of Resilience), kJ/m3 230
65 to 850
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 23
47
Strength to Weight: Axial, points 25
19 to 38
Strength to Weight: Bending, points 22
26 to 41
Thermal Diffusivity, mm2/s 2.6
54 to 65
Thermal Shock Resistance, points 19
8.7 to 18

Alloy Composition

Aluminum (Al), % 0
91 to 94.7
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20.5 to 23
0.060 to 0.2
Cobalt (Co), % 0.5 to 2.5
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 17 to 20
0 to 0.4
Magnesium (Mg), % 0
1.0 to 1.8
Manganese (Mn), % 0 to 1.0
0.2 to 0.7
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 42.3 to 54
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.35
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0.010 to 0.060
Tungsten (W), % 0.2 to 1.0
0
Zinc (Zn), % 0
4.0 to 5.0
Zirconium (Zr), % 0
0.080 to 0.2
Residuals, % 0
0 to 0.15