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EN AC-43500 Aluminum vs. EN 1.4980 Stainless Steel

EN AC-43500 aluminum belongs to the aluminum alloys classification, while EN 1.4980 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 EN AC-43500 aluminum and the bottom bar is EN 1.4980 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 4.5 to 13
17
Fatigue Strength, MPa 62 to 100
410
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
75
Tensile Strength: Ultimate (UTS), MPa 220 to 300
1030
Tensile Strength: Yield (Proof), MPa 140 to 170
680

Thermal Properties

Latent Heat of Fusion, J/g 550
300
Maximum Temperature: Mechanical, °C 170
920
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 590
1380
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
13
Thermal Expansion, µm/m-K 22
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
26
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.8
6.0
Embodied Energy, MJ/kg 150
87
Embodied Water, L/kg 1070
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 26
150
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 200
1180
Stiffness to Weight: Axial, points 16
14
Stiffness to Weight: Bending, points 54
24
Strength to Weight: Axial, points 24 to 33
36
Strength to Weight: Bending, points 32 to 39
28
Thermal Diffusivity, mm2/s 60
3.5
Thermal Shock Resistance, points 10 to 14
22

Alloy Composition


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Aluminum (Al), % 86.4 to 90.5
0 to 0.35
Boron (B), % 0
0.0030 to 0.010
Carbon (C), % 0
0.030 to 0.080
Chromium (Cr), % 0
13.5 to 16
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.25
49.2 to 58.5
Magnesium (Mg), % 0.1 to 0.6
0
Manganese (Mn), % 0.4 to 0.8
1.0 to 2.0
Molybdenum (Mo), % 0
1.0 to 1.5
Nickel (Ni), % 0
24 to 27
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 9.0 to 11.5
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.2
1.9 to 2.3
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.15
0