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EN 1.0503 Steel vs. 1200 Aluminum

EN 1.0503 steel belongs to the iron alloys classification, while 1200 aluminum belongs to the aluminum 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 EN 1.0503 steel and the bottom bar is 1200 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 180
23 to 48
Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 16
1.1 to 28
Fatigue Strength, MPa 210
25 to 69
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 380
54 to 100
Tensile Strength: Ultimate (UTS), MPa 630
85 to 180
Tensile Strength: Yield (Proof), MPa 310
28 to 160

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 400
170
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1420
650
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 48
230
Thermal Expansion, µm/m-K 12
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
58
Electrical Conductivity: Equal Weight (Specific), % IACS 8.3
190

Otherwise Unclassified Properties

Base Metal Price, % relative 2.1
9.0
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.4
8.2
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 47
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 260
5.7 to 180
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 22
8.7 to 19
Strength to Weight: Bending, points 21
16 to 26
Thermal Diffusivity, mm2/s 13
92
Thermal Shock Resistance, points 20
3.8 to 8.1

Alloy Composition


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Aluminum (Al), % 0
99 to 100
Carbon (C), % 0.42 to 0.5
0
Chromium (Cr), % 0 to 0.4
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 97.3 to 99.08
0 to 1.0
Manganese (Mn), % 0.5 to 0.8
0 to 0.050
Molybdenum (Mo), % 0 to 0.1
0
Nickel (Ni), % 0 to 0.4
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0 to 0.045
0
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15