MakeItFrom.com
Menu (ESC)

6360 Aluminum vs. EN 1.6554 Steel

6360 aluminum belongs to the aluminum alloys classification, while EN 1.6554 steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 1.6554 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 9.0 to 18
17 to 21
Fatigue Strength, MPa 31 to 67
380 to 520
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 120 to 220
780 to 930
Tensile Strength: Yield (Proof), MPa 57 to 170
550 to 790

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 160
420
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 630
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 180
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.4
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.7
Embodied Energy, MJ/kg 150
22
Embodied Water, L/kg 1190
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
140 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 24 to 210
810 to 1650
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 13 to 23
27 to 33
Strength to Weight: Bending, points 20 to 30
24 to 27
Thermal Diffusivity, mm2/s 86
11
Thermal Shock Resistance, points 5.5 to 9.9
23 to 27

Alloy Composition

Aluminum (Al), % 97.8 to 99.3
0
Carbon (C), % 0
0.23 to 0.28
Chromium (Cr), % 0 to 0.050
0.7 to 0.9
Copper (Cu), % 0 to 0.15
0 to 0.3
Iron (Fe), % 0.1 to 0.3
94.6 to 97.3
Magnesium (Mg), % 0.25 to 0.45
0
Manganese (Mn), % 0.020 to 0.15
0.6 to 0.9
Molybdenum (Mo), % 0
0.2 to 0.3
Nickel (Ni), % 0
1.0 to 2.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.35 to 0.8
0 to 0.6
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0

Comparable Variants