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Monel K-500 vs. 1080A Aluminum

Monel K-500 belongs to the nickel alloys classification, while 1080A aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 K-500 and the bottom bar is 1080A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
68
Elongation at Break, % 25 to 36
2.3 to 34
Fatigue Strength, MPa 260 to 560
18 to 50
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 61
26
Shear Strength, MPa 430 to 700
49 to 81
Tensile Strength: Ultimate (UTS), MPa 640 to 1100
74 to 140
Tensile Strength: Yield (Proof), MPa 310 to 880
17 to 120

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 900
170
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1320
640
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 18
230
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.1
62
Electrical Conductivity: Equal Weight (Specific), % IACS 3.2
200

Otherwise Unclassified Properties

Base Metal Price, % relative 50
9.5
Density, g/cm3 8.7
2.7
Embodied Carbon, kg CO2/kg material 8.1
8.3
Embodied Energy, MJ/kg 120
160
Embodied Water, L/kg 280
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180 to 260
3.1 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 2420
2.1 to 100
Stiffness to Weight: Axial, points 10
14
Stiffness to Weight: Bending, points 21
50
Strength to Weight: Axial, points 21 to 35
7.6 to 15
Strength to Weight: Bending, points 19 to 27
14 to 22
Thermal Diffusivity, mm2/s 4.8
94
Thermal Shock Resistance, points 21 to 36
3.3 to 6.4

Alloy Composition

Aluminum (Al), % 2.3 to 3.2
99.8 to 100
Carbon (C), % 0 to 0.18
0
Copper (Cu), % 27 to 33
0 to 0.030
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 0 to 2.0
0 to 0.15
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 0 to 1.5
0 to 0.020
Nickel (Ni), % 63 to 70.4
0
Silicon (Si), % 0 to 0.5
0 to 0.15
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.35 to 0.85
0 to 0.020
Zinc (Zn), % 0
0 to 0.060

Comparable Variants