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5051A Aluminum vs. Monel R-405

5051A 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 (1, 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 5051A 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, % 18 to 21
9.1 to 39
Fatigue Strength, MPa 51 to 61
210 to 250
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
62
Shear Strength, MPa 110
350 to 370
Tensile Strength: Ultimate (UTS), MPa 170
540 to 630
Tensile Strength: Yield (Proof), MPa 56
190 to 350

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 190
900
Melting Completion (Liquidus), °C 640
1350
Melting Onset (Solidus), °C 610
1300
Specific Heat Capacity, J/kg-K 900
430
Thermal Conductivity, W/m-K 150
23
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
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 8.5
7.9
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1190
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 27
49 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 23
120 to 370
Stiffness to Weight: Axial, points 14
10
Stiffness to Weight: Bending, points 50
21
Strength to Weight: Axial, points 17 to 18
17 to 20
Strength to Weight: Bending, points 25
17 to 18
Thermal Diffusivity, mm2/s 63
5.9
Thermal Shock Resistance, points 7.6
17 to 20

Alloy Composition

Aluminum (Al), % 96.1 to 98.6
0
Carbon (C), % 0
0 to 0.3
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.050
28 to 34
Iron (Fe), % 0 to 0.45
0 to 2.5
Magnesium (Mg), % 1.4 to 2.1
0
Manganese (Mn), % 0 to 0.25
0 to 2.0
Nickel (Ni), % 0
63 to 72
Silicon (Si), % 0 to 0.3
0 to 0.5
Sulfur (S), % 0
0.025 to 0.060
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0

Comparable Variants