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1200 Aluminum vs. EN 1.0503 Steel

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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