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EN AC-48100 Aluminum vs. EN 2.4889 Nickel

EN AC-48100 aluminum belongs to the aluminum alloys classification, while EN 2.4889 nickel belongs to the nickel alloys. There are 30 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 EN AC-48100 aluminum and the bottom bar is EN 2.4889 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 140
190
Elastic (Young's, Tensile) Modulus, GPa 76
200
Elongation at Break, % 1.1
39
Fatigue Strength, MPa 120 to 130
210
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 29
77
Tensile Strength: Ultimate (UTS), MPa 240 to 330
720
Tensile Strength: Yield (Proof), MPa 190 to 300
270

Thermal Properties

Latent Heat of Fusion, J/g 640
350
Maximum Temperature: Mechanical, °C 170
1200
Melting Completion (Liquidus), °C 580
1350
Melting Onset (Solidus), °C 470
1300
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 130
13
Thermal Expansion, µm/m-K 20
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 87
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
42
Density, g/cm3 2.8
8.0
Embodied Carbon, kg CO2/kg material 7.3
6.9
Embodied Energy, MJ/kg 130
98
Embodied Water, L/kg 940
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
220
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
180
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 24 to 33
25
Strength to Weight: Bending, points 31 to 38
22
Thermal Diffusivity, mm2/s 55
3.4
Thermal Shock Resistance, points 11 to 16
19

Alloy Composition

Aluminum (Al), % 72.1 to 79.8
0
Carbon (C), % 0
0.050 to 0.12
Cerium (Ce), % 0
0.030 to 0.090
Chromium (Cr), % 0
26 to 29
Copper (Cu), % 4.0 to 5.0
0 to 0.3
Iron (Fe), % 0 to 1.3
21 to 25
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0 to 1.0
Nickel (Ni), % 0 to 0.3
45 to 50.4
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 16 to 18
2.5 to 3.0
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.25
0