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5657 Aluminum vs. ASTM Grade LC2-1 Steel

5657 aluminum belongs to the aluminum alloys classification, while ASTM grade LC2-1 steel belongs to the iron alloys. There are 30 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 5657 aluminum and the bottom bar is ASTM grade LC2-1 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 50
240
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.6 to 15
20
Fatigue Strength, MPa 74 to 88
430
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 150 to 200
810
Tensile Strength: Yield (Proof), MPa 140 to 170
630

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 180
450
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 640
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
46
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
8.0
Electrical Conductivity: Equal Weight (Specific), % IACS 180
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
5.0
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.4
1.9
Embodied Energy, MJ/kg 160
25
Embodied Water, L/kg 1200
60

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.7 to 27
150
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 200
1040
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 15 to 20
29
Strength to Weight: Bending, points 23 to 28
25
Thermal Diffusivity, mm2/s 84
12
Thermal Shock Resistance, points 6.7 to 8.6
24

Alloy Composition

Aluminum (Al), % 98.5 to 99.4
0
Carbon (C), % 0
0 to 0.22
Chromium (Cr), % 0
1.4 to 1.9
Copper (Cu), % 0 to 0.1
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.1
92.5 to 95.3
Magnesium (Mg), % 0.6 to 1.0
0
Manganese (Mn), % 0 to 0.030
0.55 to 0.75
Molybdenum (Mo), % 0
0.3 to 0.6
Nickel (Ni), % 0
2.5 to 3.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.080
0 to 0.5
Sulfur (S), % 0
0 to 0.045
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.050
0