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Monel R-405 vs. 712.0 Aluminum

Monel R-405 belongs to the nickel alloys classification, while 712.0 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 712.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
70
Elongation at Break, % 9.1 to 39
4.5 to 4.7
Fatigue Strength, MPa 210 to 250
140 to 180
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 62
27
Shear Strength, MPa 350 to 370
180
Tensile Strength: Ultimate (UTS), MPa 540 to 630
250 to 260
Tensile Strength: Yield (Proof), MPa 190 to 350
180 to 200

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 900
190
Melting Completion (Liquidus), °C 1350
640
Melting Onset (Solidus), °C 1300
610
Specific Heat Capacity, J/kg-K 430
870
Thermal Conductivity, W/m-K 23
160
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
40
Electrical Conductivity: Equal Weight (Specific), % IACS 3.4
120

Otherwise Unclassified Properties

Base Metal Price, % relative 50
9.5
Density, g/cm3 8.9
3.0
Embodied Carbon, kg CO2/kg material 7.9
8.0
Embodied Energy, MJ/kg 110
150
Embodied Water, L/kg 250
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 170
11
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 370
240 to 270
Stiffness to Weight: Axial, points 10
13
Stiffness to Weight: Bending, points 21
46
Strength to Weight: Axial, points 17 to 20
24 to 25
Strength to Weight: Bending, points 17 to 18
30 to 31
Thermal Diffusivity, mm2/s 5.9
62
Thermal Shock Resistance, points 17 to 20
11

Alloy Composition


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Aluminum (Al), % 0
90.7 to 94
Carbon (C), % 0 to 0.3
0
Chromium (Cr), % 0
0.4 to 0.6
Copper (Cu), % 28 to 34
0 to 0.25
Iron (Fe), % 0 to 2.5
0 to 0.5
Magnesium (Mg), % 0
0.5 to 0.65
Manganese (Mn), % 0 to 2.0
0 to 0.1
Nickel (Ni), % 63 to 72
0
Silicon (Si), % 0 to 0.5
0 to 0.3
Sulfur (S), % 0.025 to 0.060
0
Titanium (Ti), % 0
0.15 to 0.25
Zinc (Zn), % 0
5.0 to 6.5
Residuals, % 0
0 to 0.2