MakeItFrom.com
Menu (ESC)

443.0 Aluminum vs. Nickel 690

443.0 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 443.0 aluminum and the bottom bar is nickel 690.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 41
90
Elastic (Young's, Tensile) Modulus, GPa 71
200
Elongation at Break, % 5.6
3.4 to 34
Fatigue Strength, MPa 55
180 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
79
Shear Strength, MPa 96
420 to 570
Tensile Strength: Ultimate (UTS), MPa 150
640 to 990
Tensile Strength: Yield (Proof), MPa 65
250 to 760

Thermal Properties

Latent Heat of Fusion, J/g 470
320
Maximum Temperature: Mechanical, °C 180
1010
Melting Completion (Liquidus), °C 630
1380
Melting Onset (Solidus), °C 580
1340
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
14
Thermal Expansion, µm/m-K 22
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 130
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 8.0
8.2
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1120
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.9
31 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 30
160 to 1440
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 52
24
Strength to Weight: Axial, points 16
21 to 33
Strength to Weight: Bending, points 23
20 to 27
Thermal Diffusivity, mm2/s 61
3.5
Thermal Shock Resistance, points 6.9
16 to 25

Alloy Composition

Aluminum (Al), % 90.7 to 95.5
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.25
27 to 31
Copper (Cu), % 0 to 0.6
0 to 0.5
Iron (Fe), % 0 to 0.8
7.0 to 11
Magnesium (Mg), % 0 to 0.050
0
Manganese (Mn), % 0 to 0.5
0 to 0.5
Nickel (Ni), % 0
58 to 66
Silicon (Si), % 4.5 to 6.0
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.35
0