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7003 Aluminum vs. Monel R-405

7003 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 7003 aluminum and the bottom bar is Monel R-405.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
160
Elongation at Break, % 11
9.1 to 39
Fatigue Strength, MPa 130 to 150
210 to 250
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 26
62
Shear Strength, MPa 210 to 230
350 to 370
Tensile Strength: Ultimate (UTS), MPa 350 to 390
540 to 630
Tensile Strength: Yield (Proof), MPa 300 to 310
190 to 350

Thermal Properties

Latent Heat of Fusion, J/g 380
270
Maximum Temperature: Mechanical, °C 200
900
Melting Completion (Liquidus), °C 630
1350
Melting Onset (Solidus), °C 510
1300
Specific Heat Capacity, J/kg-K 870
430
Thermal Conductivity, W/m-K 150
23
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
3.4
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.9
8.9
Embodied Carbon, kg CO2/kg material 8.1
7.9
Embodied Energy, MJ/kg 150
110
Embodied Water, L/kg 1140
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 37 to 41
49 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 710
120 to 370
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 47
21
Strength to Weight: Axial, points 33 to 37
17 to 20
Strength to Weight: Bending, points 37 to 40
17 to 18
Thermal Diffusivity, mm2/s 59
5.9
Thermal Shock Resistance, points 15 to 17
17 to 20

Alloy Composition

Aluminum (Al), % 90.6 to 94.5
0
Carbon (C), % 0
0 to 0.3
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0 to 0.2
28 to 34
Iron (Fe), % 0 to 0.35
0 to 2.5
Magnesium (Mg), % 0.5 to 1.0
0
Manganese (Mn), % 0 to 0.3
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 0.2
0
Zinc (Zn), % 5.0 to 6.5
0
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0 to 0.15
0