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7475 Aluminum vs. N10665 Nickel

7475 aluminum belongs to the aluminum alloys classification, while N10665 nickel belongs to the nickel 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 7475 aluminum and the bottom bar is N10665 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
220
Elongation at Break, % 10 to 12
45
Fatigue Strength, MPa 190 to 210
340
Poisson's Ratio 0.32
0.31
Shear Modulus, GPa 26
84
Shear Strength, MPa 320 to 350
600
Tensile Strength: Ultimate (UTS), MPa 530 to 590
860
Tensile Strength: Yield (Proof), MPa 440 to 520
400

Thermal Properties

Latent Heat of Fusion, J/g 380
310
Maximum Temperature: Mechanical, °C 180
900
Melting Completion (Liquidus), °C 640
1620
Melting Onset (Solidus), °C 480
1570
Specific Heat Capacity, J/kg-K 870
390
Thermal Conductivity, W/m-K 140 to 160
11
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 42
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 98 to 120
1.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
75
Density, g/cm3 3.0
9.3
Embodied Carbon, kg CO2/kg material 8.2
15
Embodied Energy, MJ/kg 150
200
Embodied Water, L/kg 1130
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 53 to 68
320
Resilience: Unit (Modulus of Resilience), kJ/m3 1390 to 1920
360
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
22
Strength to Weight: Axial, points 49 to 55
26
Strength to Weight: Bending, points 48 to 52
22
Thermal Diffusivity, mm2/s 53 to 63
3.1
Thermal Shock Resistance, points 23 to 26
27

Alloy Composition

Aluminum (Al), % 88.6 to 91.6
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0.18 to 0.25
0 to 1.0
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 1.2 to 1.9
0
Iron (Fe), % 0 to 0.12
0 to 2.0
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.060
0 to 1.0
Molybdenum (Mo), % 0
26 to 30
Nickel (Ni), % 0
64.8 to 74
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 0.1
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.1 to 6.2
0
Residuals, % 0 to 0.15
0