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EN 1.6579 Steel vs. 3003 Aluminum

EN 1.6579 steel belongs to the iron alloys classification, while 3003 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 1.6579 steel and the bottom bar is 3003 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 260 to 290
28 to 65
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 11 to 14
1.1 to 28
Fatigue Strength, MPa 380 to 570
39 to 90
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Tensile Strength: Ultimate (UTS), MPa 850 to 980
110 to 240
Tensile Strength: Yield (Proof), MPa 600 to 910
40 to 210

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 440
180
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1410
640
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 39
180
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.7
44
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
140

Otherwise Unclassified Properties

Base Metal Price, % relative 3.7
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 1.7
8.1
Embodied Energy, MJ/kg 22
150
Embodied Water, L/kg 56
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 100 to 120
0.95 to 63
Resilience: Unit (Modulus of Resilience), kJ/m3 950 to 2210
11 to 300
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 30 to 35
11 to 24
Strength to Weight: Bending, points 25 to 28
18 to 30
Thermal Diffusivity, mm2/s 11
71
Thermal Shock Resistance, points 25 to 29
4.7 to 10

Alloy Composition

Aluminum (Al), % 0
96.8 to 99
Carbon (C), % 0.32 to 0.38
0
Chromium (Cr), % 1.4 to 1.7
0
Copper (Cu), % 0
0.050 to 0.2
Iron (Fe), % 94.2 to 96.1
0 to 0.7
Manganese (Mn), % 0.6 to 1.0
1.0 to 1.5
Molybdenum (Mo), % 0.15 to 0.35
0
Nickel (Ni), % 1.4 to 1.7
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.6
0 to 0.6
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15

Comparable Variants