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7003 Aluminum vs. Monel K-500

7003 aluminum belongs to the aluminum alloys classification, while Monel K-500 belongs to the nickel 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 7003 aluminum and the bottom bar is Monel K-500.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
160
Elongation at Break, % 11
25 to 36
Fatigue Strength, MPa 130 to 150
260 to 560
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 26
61
Shear Strength, MPa 210 to 230
430 to 700
Tensile Strength: Ultimate (UTS), MPa 350 to 390
640 to 1100
Tensile Strength: Yield (Proof), MPa 300 to 310
310 to 880

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
1320
Specific Heat Capacity, J/kg-K 870
440
Thermal Conductivity, W/m-K 150
18
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
3.1
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.9
8.7
Embodied Carbon, kg CO2/kg material 8.1
8.1
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1140
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 37 to 41
180 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 710
300 to 2420
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 47
21
Strength to Weight: Axial, points 33 to 37
21 to 35
Strength to Weight: Bending, points 37 to 40
19 to 27
Thermal Diffusivity, mm2/s 59
4.8
Thermal Shock Resistance, points 15 to 17
21 to 36

Alloy Composition

Aluminum (Al), % 90.6 to 94.5
2.3 to 3.2
Carbon (C), % 0
0 to 0.18
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0 to 0.2
27 to 33
Iron (Fe), % 0 to 0.35
0 to 2.0
Magnesium (Mg), % 0.5 to 1.0
0
Manganese (Mn), % 0 to 0.3
0 to 1.5
Nickel (Ni), % 0
63 to 70.4
Silicon (Si), % 0 to 0.3
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0.35 to 0.85
Zinc (Zn), % 5.0 to 6.5
0
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0 to 0.15
0