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1080A Aluminum vs. EN 1.8912 Steel

1080A aluminum belongs to the aluminum alloys classification, while EN 1.8912 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 1080A aluminum and the bottom bar is EN 1.8912 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 18 to 40
180
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 2.3 to 34
20
Fatigue Strength, MPa 18 to 50
290
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 49 to 81
380
Tensile Strength: Ultimate (UTS), MPa 74 to 140
600
Tensile Strength: Yield (Proof), MPa 17 to 120
410

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 170
410
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 640
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 230
46
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 62
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 200
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.6
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.8
Embodied Energy, MJ/kg 160
24
Embodied Water, L/kg 1200
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.1 to 19
110
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 100
460
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.6 to 15
21
Strength to Weight: Bending, points 14 to 22
20
Thermal Diffusivity, mm2/s 94
12
Thermal Shock Resistance, points 3.3 to 6.4
18

Alloy Composition

Aluminum (Al), % 99.8 to 100
0 to 0.015
Carbon (C), % 0
0 to 0.22
Chromium (Cr), % 0
0 to 0.35
Copper (Cu), % 0 to 0.030
0 to 0.6
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.15
95 to 99.05
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0 to 0.020
1.0 to 1.8
Molybdenum (Mo), % 0
0 to 0.13
Nickel (Ni), % 0
0 to 0.85
Niobium (Nb), % 0
0 to 0.060
Nitrogen (N), % 0
0 to 0.027
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.15
0 to 0.65
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.020
0 to 0.060
Vanadium (V), % 0
0 to 0.22
Zinc (Zn), % 0 to 0.060
0