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N10665 Nickel vs. 7475 Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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