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Nickel 690 vs. 5182 Aluminum

Nickel 690 belongs to the nickel alloys classification, while 5182 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 nickel 690 and the bottom bar is 5182 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 3.4 to 34
1.1 to 12
Fatigue Strength, MPa 180 to 300
100 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 79
25
Shear Strength, MPa 420 to 570
170 to 240
Tensile Strength: Ultimate (UTS), MPa 640 to 990
280 to 420
Tensile Strength: Yield (Proof), MPa 250 to 760
130 to 360

Thermal Properties

Latent Heat of Fusion, J/g 320
390
Maximum Temperature: Mechanical, °C 1010
180
Melting Completion (Liquidus), °C 1380
640
Melting Onset (Solidus), °C 1340
590
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 14
130
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
28
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
94

Otherwise Unclassified Properties

Base Metal Price, % relative 50
9.5
Density, g/cm3 8.3
2.7
Embodied Carbon, kg CO2/kg material 8.2
8.9
Embodied Energy, MJ/kg 120
150
Embodied Water, L/kg 290
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 170
2.6 to 49
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 1440
120 to 950
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 21 to 33
29 to 44
Strength to Weight: Bending, points 20 to 27
36 to 47
Thermal Diffusivity, mm2/s 3.5
53
Thermal Shock Resistance, points 16 to 25
12 to 19

Alloy Composition

Aluminum (Al), % 0
93.2 to 95.8
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 27 to 31
0 to 0.1
Copper (Cu), % 0 to 0.5
0 to 0.15
Iron (Fe), % 7.0 to 11
0 to 0.35
Magnesium (Mg), % 0
4.0 to 5.0
Manganese (Mn), % 0 to 0.5
0.2 to 0.5
Nickel (Ni), % 58 to 66
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants