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EN AC-48000 Aluminum vs. EN 1.4361 Stainless Steel

EN AC-48000 aluminum belongs to the aluminum alloys classification, while EN 1.4361 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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-48000 aluminum and the bottom bar is EN 1.4361 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 110
200
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 1.0
43
Fatigue Strength, MPa 85 to 86
220
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
75
Tensile Strength: Ultimate (UTS), MPa 220 to 310
630
Tensile Strength: Yield (Proof), MPa 210 to 270
250

Thermal Properties

Latent Heat of Fusion, J/g 570
350
Maximum Temperature: Mechanical, °C 190
940
Melting Completion (Liquidus), °C 600
1370
Melting Onset (Solidus), °C 560
1330
Specific Heat Capacity, J/kg-K 890
490
Thermal Conductivity, W/m-K 130
14
Thermal Expansion, µm/m-K 21
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
2.1
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 10
19
Density, g/cm3 2.7
7.6
Embodied Carbon, kg CO2/kg material 7.9
3.6
Embodied Energy, MJ/kg 140
52
Embodied Water, L/kg 1030
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.2 to 3.0
220
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 510
160
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 23 to 33
23
Strength to Weight: Bending, points 31 to 39
21
Thermal Diffusivity, mm2/s 54
3.7
Thermal Shock Resistance, points 10 to 15
15

Alloy Composition

Aluminum (Al), % 80.4 to 87.2
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0
16.5 to 18.5
Copper (Cu), % 0.8 to 1.5
0
Iron (Fe), % 0 to 0.7
58.7 to 65.8
Magnesium (Mg), % 0.8 to 1.5
0
Manganese (Mn), % 0 to 0.35
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.2
Nickel (Ni), % 0.7 to 1.3
14 to 16
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 10.5 to 13.5
3.7 to 4.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0