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1080A Aluminum vs. Monel R-405

1080A aluminum belongs to the aluminum alloys classification, while Monel R-405 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 1080A aluminum and the bottom bar is Monel R-405.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
160
Elongation at Break, % 2.3 to 34
9.1 to 39
Fatigue Strength, MPa 18 to 50
210 to 250
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
62
Shear Strength, MPa 49 to 81
350 to 370
Tensile Strength: Ultimate (UTS), MPa 74 to 140
540 to 630
Tensile Strength: Yield (Proof), MPa 17 to 120
190 to 350

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 640
1300
Specific Heat Capacity, J/kg-K 900
430
Thermal Conductivity, W/m-K 230
23
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 62
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 200
3.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.9
Embodied Carbon, kg CO2/kg material 8.3
7.9
Embodied Energy, MJ/kg 160
110
Embodied Water, L/kg 1200
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.1 to 19
49 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 100
120 to 370
Stiffness to Weight: Axial, points 14
10
Stiffness to Weight: Bending, points 50
21
Strength to Weight: Axial, points 7.6 to 15
17 to 20
Strength to Weight: Bending, points 14 to 22
17 to 18
Thermal Diffusivity, mm2/s 94
5.9
Thermal Shock Resistance, points 3.3 to 6.4
17 to 20

Alloy Composition

Aluminum (Al), % 99.8 to 100
0
Carbon (C), % 0
0 to 0.3
Copper (Cu), % 0 to 0.030
28 to 34
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.15
0 to 2.5
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0 to 0.020
0 to 2.0
Nickel (Ni), % 0
63 to 72
Silicon (Si), % 0 to 0.15
0 to 0.5
Sulfur (S), % 0
0.025 to 0.060
Titanium (Ti), % 0 to 0.020
0
Zinc (Zn), % 0 to 0.060
0

Comparable Variants