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N06230 Nickel vs. EN AC-45300 Aluminum

N06230 nickel belongs to the nickel alloys classification, while EN AC-45300 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 N06230 nickel and the bottom bar is EN AC-45300 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
71
Elongation at Break, % 38 to 48
1.0 to 2.8
Fatigue Strength, MPa 250 to 360
59 to 72
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 83
27
Tensile Strength: Ultimate (UTS), MPa 620 to 840
220 to 290
Tensile Strength: Yield (Proof), MPa 330 to 400
150 to 230

Thermal Properties

Latent Heat of Fusion, J/g 310
470
Maximum Temperature: Mechanical, °C 990
170
Melting Completion (Liquidus), °C 1370
630
Melting Onset (Solidus), °C 1300
590
Specific Heat Capacity, J/kg-K 420
890
Thermal Conductivity, W/m-K 8.9
150
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
36
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
120

Otherwise Unclassified Properties

Base Metal Price, % relative 85
9.5
Density, g/cm3 9.5
2.7
Embodied Carbon, kg CO2/kg material 11
8.0
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 290
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
2.7 to 5.6
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
160 to 390
Stiffness to Weight: Axial, points 12
14
Stiffness to Weight: Bending, points 21
50
Strength to Weight: Axial, points 18 to 25
23 to 29
Strength to Weight: Bending, points 17 to 21
30 to 35
Thermal Diffusivity, mm2/s 2.3
60
Thermal Shock Resistance, points 17 to 23
10 to 13

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
90.2 to 94.2
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20 to 24
0
Cobalt (Co), % 0 to 5.0
0
Copper (Cu), % 0
1.0 to 1.5
Iron (Fe), % 0 to 3.0
0 to 0.65
Lanthanum (La), % 0.0050 to 0.050
0
Lead (Pb), % 0
0 to 0.15
Magnesium (Mg), % 0
0.35 to 0.65
Manganese (Mn), % 0.3 to 1.0
0 to 0.55
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0 to 0.25
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
4.5 to 5.5
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0
0 to 0.25
Tungsten (W), % 13 to 15
0
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15