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EN AC-42100 Aluminum vs. EN 1.4854 Stainless Steel

EN AC-42100 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-42100 aluminum and the bottom bar is EN 1.4854 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 91
180
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 3.4 to 9.0
45
Fatigue Strength, MPa 76 to 82
310
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Tensile Strength: Ultimate (UTS), MPa 280 to 290
750
Tensile Strength: Yield (Proof), MPa 210 to 230
340

Thermal Properties

Latent Heat of Fusion, J/g 500
330
Maximum Temperature: Mechanical, °C 170
1170
Melting Completion (Liquidus), °C 610
1370
Melting Onset (Solidus), °C 600
1330
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 150
11
Thermal Expansion, µm/m-K 22
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 140
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 8.0
5.7
Embodied Energy, MJ/kg 150
81
Embodied Water, L/kg 1110
220

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.1 to 23
270
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 370
280
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 30 to 31
26
Strength to Weight: Bending, points 37 to 38
23
Thermal Diffusivity, mm2/s 66
2.9
Thermal Shock Resistance, points 13
18

Alloy Composition


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Aluminum (Al), % 91.3 to 93.3
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 0.19
33.6 to 40.6
Magnesium (Mg), % 0.25 to 0.45
0
Manganese (Mn), % 0 to 0.1
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), % 6.5 to 7.5
1.2 to 2.0
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