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5182 Aluminum vs. Monel K-500

5182 aluminum belongs to the aluminum alloys classification, while Monel K-500 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 5182 aluminum and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
160
Elongation at Break, % 1.1 to 12
25 to 36
Fatigue Strength, MPa 100 to 130
260 to 560
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 25
61
Shear Strength, MPa 170 to 240
430 to 700
Tensile Strength: Ultimate (UTS), MPa 280 to 420
640 to 1100
Tensile Strength: Yield (Proof), MPa 130 to 360
310 to 880

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 180
900
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 590
1320
Specific Heat Capacity, J/kg-K 900
440
Thermal Conductivity, W/m-K 130
18
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 94
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.7
Embodied Carbon, kg CO2/kg material 8.9
8.1
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1180
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.6 to 49
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 950
300 to 2420
Stiffness to Weight: Axial, points 14
10
Stiffness to Weight: Bending, points 51
21
Strength to Weight: Axial, points 29 to 44
21 to 35
Strength to Weight: Bending, points 36 to 47
19 to 27
Thermal Diffusivity, mm2/s 53
4.8
Thermal Shock Resistance, points 12 to 19
21 to 36

Alloy Composition

Aluminum (Al), % 93.2 to 95.8
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.15
27 to 33
Iron (Fe), % 0 to 0.35
0 to 2.0
Magnesium (Mg), % 4.0 to 5.0
0
Manganese (Mn), % 0.2 to 0.5
0 to 1.5
Nickel (Ni), % 0
63 to 70.4
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0.35 to 0.85
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0

Comparable Variants