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5005 Aluminum vs. Nickel 690

5005 aluminum belongs to the aluminum alloys classification, while nickel 690 belongs to the nickel alloys. There are 31 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 5005 aluminum and the bottom bar is nickel 690.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 28 to 64
90
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.1 to 23
3.4 to 34
Fatigue Strength, MPa 38 to 86
180 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
79
Shear Strength, MPa 70 to 130
420 to 570
Tensile Strength: Ultimate (UTS), MPa 110 to 230
640 to 990
Tensile Strength: Yield (Proof), MPa 41 to 210
250 to 760

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 180
1010
Melting Completion (Liquidus), °C 650
1380
Melting Onset (Solidus), °C 630
1340
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 200
14
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 52
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 170
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.3
8.2
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1190
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 22
31 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 12 to 320
160 to 1440
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 11 to 23
21 to 33
Strength to Weight: Bending, points 19 to 31
20 to 27
Thermal Diffusivity, mm2/s 82
3.5
Thermal Shock Resistance, points 4.9 to 10
16 to 25

Alloy Composition

Aluminum (Al), % 97 to 99.5
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.1
27 to 31
Copper (Cu), % 0 to 0.2
0 to 0.5
Iron (Fe), % 0 to 0.7
7.0 to 11
Magnesium (Mg), % 0.5 to 1.1
0
Manganese (Mn), % 0 to 0.2
0 to 0.5
Nickel (Ni), % 0
58 to 66
Silicon (Si), % 0 to 0.3
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants