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EN AC-48000 Aluminum vs. Monel K-500

EN AC-48000 aluminum belongs to the aluminum alloys classification, while Monel K-500 belongs to the nickel 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 EN AC-48000 aluminum and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
160
Elongation at Break, % 1.0
25 to 36
Fatigue Strength, MPa 85 to 86
260 to 560
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 28
61
Tensile Strength: Ultimate (UTS), MPa 220 to 310
640 to 1100
Tensile Strength: Yield (Proof), MPa 210 to 270
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 570
270
Maximum Temperature: Mechanical, °C 190
900
Melting Completion (Liquidus), °C 600
1350
Melting Onset (Solidus), °C 560
1320
Specific Heat Capacity, J/kg-K 890
440
Thermal Conductivity, W/m-K 130
18
Thermal Expansion, µm/m-K 21
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
50
Density, g/cm3 2.7
8.7
Embodied Carbon, kg CO2/kg material 7.9
8.1
Embodied Energy, MJ/kg 140
120
Embodied Water, L/kg 1030
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.2 to 3.0
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 510
300 to 2420
Stiffness to Weight: Axial, points 15
10
Stiffness to Weight: Bending, points 53
21
Strength to Weight: Axial, points 23 to 33
21 to 35
Strength to Weight: Bending, points 31 to 39
19 to 27
Thermal Diffusivity, mm2/s 54
4.8
Thermal Shock Resistance, points 10 to 15
21 to 36

Alloy Composition

Aluminum (Al), % 80.4 to 87.2
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Copper (Cu), % 0.8 to 1.5
27 to 33
Iron (Fe), % 0 to 0.7
0 to 2.0
Magnesium (Mg), % 0.8 to 1.5
0
Manganese (Mn), % 0 to 0.35
0 to 1.5
Nickel (Ni), % 0.7 to 1.3
63 to 70.4
Silicon (Si), % 10.5 to 13.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0.35 to 0.85
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0