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EN AC-43500 Aluminum vs. EN 1.4854 Stainless Steel

EN AC-43500 aluminum belongs to the aluminum alloys classification, while EN 1.4854 stainless steel belongs to the iron 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 EN AC-43500 aluminum and the bottom bar is EN 1.4854 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 68 to 91
180
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 4.5 to 13
45
Fatigue Strength, MPa 62 to 100
310
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Tensile Strength: Ultimate (UTS), MPa 220 to 300
750
Tensile Strength: Yield (Proof), MPa 140 to 170
340

Thermal Properties

Latent Heat of Fusion, J/g 550
330
Maximum Temperature: Mechanical, °C 170
1170
Melting Completion (Liquidus), °C 600
1370
Melting Onset (Solidus), °C 590
1330
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 140
11
Thermal Expansion, µm/m-K 22
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
34
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.8
5.7
Embodied Energy, MJ/kg 150
81
Embodied Water, L/kg 1070
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 26
270
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 200
280
Stiffness to Weight: Axial, points 16
14
Stiffness to Weight: Bending, points 54
25
Strength to Weight: Axial, points 24 to 33
26
Strength to Weight: Bending, points 32 to 39
23
Thermal Diffusivity, mm2/s 60
2.9
Thermal Shock Resistance, points 10 to 14
18

Alloy Composition

Aluminum (Al), % 86.4 to 90.5
0
Carbon (C), % 0
0.040 to 0.080
Cerium (Ce), % 0
0.030 to 0.080
Chromium (Cr), % 0
24 to 26
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.25
33.6 to 40.6
Magnesium (Mg), % 0.1 to 0.6
0
Manganese (Mn), % 0.4 to 0.8
0 to 2.0
Nickel (Ni), % 0
34 to 36
Nitrogen (N), % 0
0.12 to 0.2
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 9.0 to 11.5
1.2 to 2.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.15
0