MakeItFrom.com
Menu (ESC)

7475 Aluminum vs. N06455 Nickel

7475 aluminum belongs to the aluminum alloys classification, while N06455 nickel 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 7475 aluminum and the bottom bar is N06455 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 10 to 12
47
Fatigue Strength, MPa 190 to 210
290
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
82
Shear Strength, MPa 320 to 350
550
Tensile Strength: Ultimate (UTS), MPa 530 to 590
780
Tensile Strength: Yield (Proof), MPa 440 to 520
330

Thermal Properties

Latent Heat of Fusion, J/g 380
320
Maximum Temperature: Mechanical, °C 180
960
Melting Completion (Liquidus), °C 640
1510
Melting Onset (Solidus), °C 480
1450
Specific Heat Capacity, J/kg-K 870
430
Thermal Conductivity, W/m-K 140 to 160
10
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 42
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 98 to 120
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
65
Density, g/cm3 3.0
8.8
Embodied Carbon, kg CO2/kg material 8.2
12
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 1130
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 53 to 68
300
Resilience: Unit (Modulus of Resilience), kJ/m3 1390 to 1920
260
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
23
Strength to Weight: Axial, points 49 to 55
24
Strength to Weight: Bending, points 48 to 52
21
Thermal Diffusivity, mm2/s 53 to 63
2.7
Thermal Shock Resistance, points 23 to 26
24

Alloy Composition

Aluminum (Al), % 88.6 to 91.6
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0.18 to 0.25
14 to 18
Cobalt (Co), % 0
0 to 2.0
Copper (Cu), % 1.2 to 1.9
0
Iron (Fe), % 0 to 0.12
0 to 3.0
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.060
0 to 1.0
Molybdenum (Mo), % 0
14 to 17
Nickel (Ni), % 0
58.1 to 72
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 0.080
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0 to 0.7
Zinc (Zn), % 5.1 to 6.2
0
Residuals, % 0 to 0.15
0