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EN AC-42100 Aluminum vs. EN 1.4841 Stainless Steel

EN AC-42100 aluminum belongs to the aluminum alloys classification, while EN 1.4841 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-42100 aluminum and the bottom bar is EN 1.4841 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 91
190
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 3.4 to 9.0
32
Fatigue Strength, MPa 76 to 82
200
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Tensile Strength: Ultimate (UTS), MPa 280 to 290
650
Tensile Strength: Yield (Proof), MPa 210 to 230
260

Thermal Properties

Latent Heat of Fusion, J/g 500
330
Maximum Temperature: Mechanical, °C 170
1150
Melting Completion (Liquidus), °C 610
1380
Melting Onset (Solidus), °C 600
1340
Specific Heat Capacity, J/kg-K 910
490
Thermal Conductivity, W/m-K 150
15
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
25
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 8.0
4.3
Embodied Energy, MJ/kg 150
62
Embodied Water, L/kg 1110
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.1 to 23
170
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 370
170
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 30 to 31
23
Strength to Weight: Bending, points 37 to 38
21
Thermal Diffusivity, mm2/s 66
4.0
Thermal Shock Resistance, points 13
15

Alloy Composition


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Aluminum (Al), % 91.3 to 93.3
0
Carbon (C), % 0
0 to 0.2
Chromium (Cr), % 0
24 to 26
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.19
47.1 to 55.5
Magnesium (Mg), % 0.25 to 0.45
0
Manganese (Mn), % 0 to 0.1
0 to 2.0
Nickel (Ni), % 0
19 to 22
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 6.5 to 7.5
1.5 to 2.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.1
0