MakeItFrom.com
Menu (ESC)

8090 Aluminum vs. Nickel 690

8090 aluminum belongs to the aluminum alloys classification, while nickel 690 belongs to the nickel alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 8090 aluminum and the bottom bar is nickel 690.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 3.5 to 13
3.4 to 34
Fatigue Strength, MPa 91 to 140
180 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
79
Tensile Strength: Ultimate (UTS), MPa 340 to 490
640 to 990
Tensile Strength: Yield (Proof), MPa 210 to 420
250 to 760

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 190
1010
Melting Completion (Liquidus), °C 660
1380
Melting Onset (Solidus), °C 600
1340
Specific Heat Capacity, J/kg-K 960
470
Thermal Conductivity, W/m-K 95 to 160
14
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 66
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 18
50
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.6
8.2
Embodied Energy, MJ/kg 170
120
Embodied Water, L/kg 1160
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 41
31 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 340 to 1330
160 to 1440
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 34 to 49
21 to 33
Strength to Weight: Bending, points 39 to 50
20 to 27
Thermal Diffusivity, mm2/s 36 to 60
3.5
Thermal Shock Resistance, points 15 to 22
16 to 25

Alloy Composition

Aluminum (Al), % 93 to 98.4
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.1
27 to 31
Copper (Cu), % 1.0 to 1.6
0 to 0.5
Iron (Fe), % 0 to 0.3
7.0 to 11
Lithium (Li), % 2.2 to 2.7
0
Magnesium (Mg), % 0.6 to 1.3
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Nickel (Ni), % 0
58 to 66
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0.040 to 0.16
0
Residuals, % 0 to 0.15
0