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Nickel 600 vs. EN AC-43300 Aluminum

Nickel 600 belongs to the nickel alloys classification, while EN AC-43300 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 600 and the bottom bar is EN AC-43300 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 3.4 to 35
3.4 to 6.7
Fatigue Strength, MPa 220 to 300
76 to 77
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
27
Tensile Strength: Ultimate (UTS), MPa 650 to 990
280 to 290
Tensile Strength: Yield (Proof), MPa 270 to 760
210 to 230

Thermal Properties

Latent Heat of Fusion, J/g 310
540
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1410
600
Melting Onset (Solidus), °C 1350
590
Specific Heat Capacity, J/kg-K 460
910
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
40
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
140

Otherwise Unclassified Properties

Base Metal Price, % relative 55
9.5
Density, g/cm3 8.5
2.5
Embodied Carbon, kg CO2/kg material 9.0
7.9
Embodied Energy, MJ/kg 130
150
Embodied Water, L/kg 250
1080

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 180
9.1 to 17
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 1490
300 to 370
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 23
54
Strength to Weight: Axial, points 21 to 32
31 to 32
Strength to Weight: Bending, points 20 to 26
37 to 38
Thermal Diffusivity, mm2/s 3.6
59
Thermal Shock Resistance, points 19 to 29
13 to 14

Alloy Composition

Aluminum (Al), % 0
88.9 to 90.8
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 14 to 17
0
Copper (Cu), % 0 to 0.5
0 to 0.050
Iron (Fe), % 6.0 to 10
0 to 0.19
Magnesium (Mg), % 0
0.25 to 0.45
Manganese (Mn), % 0 to 1.0
0 to 0.1
Nickel (Ni), % 72 to 80
0
Silicon (Si), % 0 to 0.5
9.0 to 10
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.070
Residuals, % 0
0 to 0.1