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Monel R-405 vs. 6005 Aluminum

Monel R-405 belongs to the nickel alloys classification, while 6005 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 R-405 and the bottom bar is 6005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
68
Elongation at Break, % 9.1 to 39
9.5 to 17
Fatigue Strength, MPa 210 to 250
55 to 95
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 62
26
Shear Strength, MPa 350 to 370
120 to 210
Tensile Strength: Ultimate (UTS), MPa 540 to 630
190 to 310
Tensile Strength: Yield (Proof), MPa 190 to 350
100 to 280

Thermal Properties

Latent Heat of Fusion, J/g 270
410
Maximum Temperature: Mechanical, °C 900
160
Melting Completion (Liquidus), °C 1350
650
Melting Onset (Solidus), °C 1300
610
Specific Heat Capacity, J/kg-K 430
900
Thermal Conductivity, W/m-K 23
180 to 200
Thermal Expansion, µm/m-K 14
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
54
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
180

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
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 170
27 to 36
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 370
77 to 550
Stiffness to Weight: Axial, points 10
14
Stiffness to Weight: Bending, points 21
51
Strength to Weight: Axial, points 17 to 20
20 to 32
Strength to Weight: Bending, points 17 to 18
28 to 38
Thermal Diffusivity, mm2/s 5.9
74 to 83
Thermal Shock Resistance, points 17 to 20
8.6 to 14

Alloy Composition

Aluminum (Al), % 0
97.5 to 99
Carbon (C), % 0 to 0.3
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 28 to 34
0 to 0.1
Iron (Fe), % 0 to 2.5
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0 to 2.0
0 to 0.1
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
0.6 to 0.9
Sulfur (S), % 0.025 to 0.060
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15