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Monel R-405 vs. 4015 Aluminum

Monel R-405 belongs to the nickel alloys classification, while 4015 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 R-405 and the bottom bar is 4015 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
70
Elongation at Break, % 9.1 to 39
1.1 to 23
Fatigue Strength, MPa 210 to 250
46 to 71
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 62
26
Shear Strength, MPa 350 to 370
82 to 120
Tensile Strength: Ultimate (UTS), MPa 540 to 630
130 to 220
Tensile Strength: Yield (Proof), MPa 190 to 350
50 to 200

Thermal Properties

Latent Heat of Fusion, J/g 270
420
Maximum Temperature: Mechanical, °C 900
160
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1300
600
Specific Heat Capacity, J/kg-K 430
900
Thermal Conductivity, W/m-K 23
160
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
41
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
130

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
8.1
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 250
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 170
2.4 to 24
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 370
18 to 290
Stiffness to Weight: Axial, points 10
14
Stiffness to Weight: Bending, points 21
50
Strength to Weight: Axial, points 17 to 20
13 to 22
Strength to Weight: Bending, points 17 to 18
21 to 30
Thermal Diffusivity, mm2/s 5.9
66
Thermal Shock Resistance, points 17 to 20
5.7 to 9.7

Alloy Composition

Aluminum (Al), % 0
94.9 to 97.9
Carbon (C), % 0 to 0.3
0
Copper (Cu), % 28 to 34
0 to 0.2
Iron (Fe), % 0 to 2.5
0 to 0.7
Magnesium (Mg), % 0
0.1 to 0.5
Manganese (Mn), % 0 to 2.0
0.6 to 1.2
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
1.4 to 2.2
Sulfur (S), % 0.025 to 0.060
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15

Comparable Variants