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EN 1.1127 Steel vs. 5021 Aluminum

EN 1.1127 steel belongs to the iron alloys classification, while 5021 aluminum belongs to the aluminum alloys. There are 30 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 1.1127 steel and the bottom bar is 5021 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 14 to 25
1.1 to 3.4
Fatigue Strength, MPa 280 to 370
85 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Shear Strength, MPa 420 to 480
170
Tensile Strength: Ultimate (UTS), MPa 660 to 790
300 to 310
Tensile Strength: Yield (Proof), MPa 410 to 580
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 400
180
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1410
590
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 49
140
Thermal Expansion, µm/m-K 12
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
120

Otherwise Unclassified Properties

Base Metal Price, % relative 2.1
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.5
8.6
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 49
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 90 to 140
3.1 to 10
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 880
440 to 550
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 23 to 28
30 to 32
Strength to Weight: Bending, points 22 to 24
37
Thermal Diffusivity, mm2/s 13
57
Thermal Shock Resistance, points 21 to 25
13 to 14

Alloy Composition

Aluminum (Al), % 0
95.2 to 97.7
Carbon (C), % 0.34 to 0.42
0
Chromium (Cr), % 0 to 0.4
0 to 0.15
Copper (Cu), % 0
0 to 0.15
Iron (Fe), % 96.6 to 98.1
0 to 0.5
Magnesium (Mg), % 0
2.2 to 2.8
Manganese (Mn), % 1.4 to 1.7
0.1 to 0.5
Molybdenum (Mo), % 0 to 0.1
0
Nickel (Ni), % 0 to 0.4
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.15 to 0.35
0 to 0.4
Sulfur (S), % 0 to 0.035
0
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15