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1070A Aluminum vs. EN 1.8880 Steel

1070A aluminum belongs to the aluminum alloys classification, while EN 1.8880 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 1070A aluminum and the bottom bar is EN 1.8880 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 18 to 40
250
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 2.3 to 33
16
Fatigue Strength, MPa 17 to 51
470
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 44 to 81
510
Tensile Strength: Ultimate (UTS), MPa 68 to 140
830
Tensile Strength: Yield (Proof), MPa 17 to 120
720

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 170
420
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
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 60
8.1
Electrical Conductivity: Equal Weight (Specific), % IACS 200
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
3.7
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.2
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1200
54

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.0 to 18
130
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 100
1370
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.0 to 14
29
Strength to Weight: Bending, points 14 to 22
25
Thermal Diffusivity, mm2/s 94
11
Thermal Shock Resistance, points 3.1 to 6.3
24

Alloy Composition

Aluminum (Al), % 99.7 to 100
0
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0
0 to 0.2
Chromium (Cr), % 0
0 to 1.5
Copper (Cu), % 0 to 0.030
0 to 0.3
Iron (Fe), % 0 to 0.25
91.9 to 100
Magnesium (Mg), % 0 to 0.030
0
Manganese (Mn), % 0 to 0.030
0 to 1.7
Molybdenum (Mo), % 0
0 to 0.7
Nickel (Ni), % 0
0 to 2.5
Niobium (Nb), % 0
0 to 0.060
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.8
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.030
0 to 0.050
Vanadium (V), % 0
0 to 0.12
Zinc (Zn), % 0 to 0.070
0
Zirconium (Zr), % 0
0 to 0.15