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6360 Aluminum vs. EN 1.1127 Steel

6360 aluminum belongs to the aluminum alloys classification, while EN 1.1127 steel belongs to the iron 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 6360 aluminum and the bottom bar is EN 1.1127 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 9.0 to 18
14 to 25
Fatigue Strength, MPa 31 to 67
280 to 370
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 76 to 130
420 to 480
Tensile Strength: Ultimate (UTS), MPa 120 to 220
660 to 790
Tensile Strength: Yield (Proof), MPa 57 to 170
410 to 580

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 160
400
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 630
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
49
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 180
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.1
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.5
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1190
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
90 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 24 to 210
440 to 880
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 13 to 23
23 to 28
Strength to Weight: Bending, points 20 to 30
22 to 24
Thermal Diffusivity, mm2/s 86
13
Thermal Shock Resistance, points 5.5 to 9.9
21 to 25

Alloy Composition

Aluminum (Al), % 97.8 to 99.3
0
Carbon (C), % 0
0.34 to 0.42
Chromium (Cr), % 0 to 0.050
0 to 0.4
Copper (Cu), % 0 to 0.15
0
Iron (Fe), % 0.1 to 0.3
96.6 to 98.1
Magnesium (Mg), % 0.25 to 0.45
0
Manganese (Mn), % 0.020 to 0.15
1.4 to 1.7
Molybdenum (Mo), % 0
0 to 0.1
Nickel (Ni), % 0
0 to 0.4
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0.35 to 0.8
0.15 to 0.35
Sulfur (S), % 0
0 to 0.035
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0