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355.0 Aluminum vs. Monel R-405

355.0 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 (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 355.0 aluminum and the bottom bar is Monel R-405.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
160
Elongation at Break, % 1.5 to 2.6
9.1 to 39
Fatigue Strength, MPa 55 to 70
210 to 250
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 27
62
Shear Strength, MPa 150 to 240
350 to 370
Tensile Strength: Ultimate (UTS), MPa 200 to 260
540 to 630
Tensile Strength: Yield (Proof), MPa 150 to 190
190 to 350

Thermal Properties

Latent Heat of Fusion, J/g 470
270
Maximum Temperature: Mechanical, °C 180
900
Melting Completion (Liquidus), °C 620
1350
Melting Onset (Solidus), °C 560
1300
Specific Heat Capacity, J/kg-K 890
430
Thermal Conductivity, W/m-K 150 to 170
23
Thermal Expansion, µm/m-K 22
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38 to 43
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 120 to 140
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 8.0
7.9
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1120
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.9
49 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 250
120 to 370
Stiffness to Weight: Axial, points 14
10
Stiffness to Weight: Bending, points 51
21
Strength to Weight: Axial, points 20 to 27
17 to 20
Strength to Weight: Bending, points 28 to 33
17 to 18
Thermal Diffusivity, mm2/s 60 to 69
5.9
Thermal Shock Resistance, points 9.1 to 12
17 to 20

Alloy Composition

Aluminum (Al), % 90.3 to 94.1
0
Carbon (C), % 0
0 to 0.3
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 1.0 to 1.5
28 to 34
Iron (Fe), % 0 to 0.6
0 to 2.5
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.5
0 to 2.0
Nickel (Ni), % 0
63 to 72
Silicon (Si), % 4.5 to 5.5
0 to 0.5
Sulfur (S), % 0
0.025 to 0.060
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0