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Monel 400 vs. 5110A Aluminum

Monel 400 belongs to the nickel alloys classification, while 5110A aluminum belongs to the aluminum 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 Monel 400 and the bottom bar is 5110A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
68
Elongation at Break, % 20 to 40
4.5 to 28
Fatigue Strength, MPa 230 to 290
37 to 77
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 62
26
Shear Strength, MPa 370 to 490
66 to 110
Tensile Strength: Ultimate (UTS), MPa 540 to 780
100 to 190
Tensile Strength: Yield (Proof), MPa 210 to 590
32 to 170

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 1000
180
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1300
640
Specific Heat Capacity, J/kg-K 430
900
Thermal Conductivity, W/m-K 23
220
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.3
57
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
190

Otherwise Unclassified Properties

Base Metal Price, % relative 50
9.5
Density, g/cm3 8.9
2.7
Embodied Carbon, kg CO2/kg material 7.9
8.3
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 250
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 180
6.8 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 1080
7.6 to 200
Stiffness to Weight: Axial, points 10
14
Stiffness to Weight: Bending, points 21
50
Strength to Weight: Axial, points 17 to 25
10 to 19
Strength to Weight: Bending, points 17 to 21
18 to 27
Thermal Diffusivity, mm2/s 6.1
91
Thermal Shock Resistance, points 17 to 25
4.5 to 8.4

Alloy Composition

Aluminum (Al), % 0
98.5 to 99.8
Carbon (C), % 0 to 0.3
0
Copper (Cu), % 28 to 34
0 to 0.2
Iron (Fe), % 0 to 2.5
0 to 0.25
Magnesium (Mg), % 0
0.2 to 0.6
Manganese (Mn), % 0 to 2.0
0 to 0.2
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
0 to 0.15
Sulfur (S), % 0 to 0.024
0
Zinc (Zn), % 0
0 to 0.030
Residuals, % 0
0 to 0.1

Comparable Variants