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1070 Aluminum vs. EN 1.7383 Steel

1070 aluminum belongs to the aluminum alloys classification, while EN 1.7383 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 1070 aluminum and the bottom bar is EN 1.7383 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 4.5 to 39
20 to 23
Fatigue Strength, MPa 22 to 49
210 to 270
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 48 to 79
350 to 380
Tensile Strength: Ultimate (UTS), MPa 73 to 140
560 to 610
Tensile Strength: Yield (Proof), MPa 17 to 120
300 to 400

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 170
460
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 640
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 230
39
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 200
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.8
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 1200
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.8 to 21
110
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 110
240 to 420
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.5 to 14
20 to 22
Strength to Weight: Bending, points 14 to 22
19 to 20
Thermal Diffusivity, mm2/s 94
11
Thermal Shock Resistance, points 3.3 to 6.1
16 to 18

Alloy Composition

Aluminum (Al), % 99.7 to 100
0 to 0.040
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0
2.0 to 2.5
Copper (Cu), % 0 to 0.040
0 to 0.3
Iron (Fe), % 0 to 0.25
94.3 to 96.6
Magnesium (Mg), % 0 to 0.030
0
Manganese (Mn), % 0 to 0.030
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.030
0
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.040
0
Residuals, % 0 to 0.030
0