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5657 Aluminum vs. EN 1.4848 Stainless Steel

5657 aluminum belongs to the aluminum alloys classification, while EN 1.4848 stainless 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 EN 1.4848 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 50
150
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.6 to 15
9.0
Fatigue Strength, MPa 74 to 88
130
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Tensile Strength: Ultimate (UTS), MPa 150 to 200
510
Tensile Strength: Yield (Proof), MPa 140 to 170
250

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 660
1390
Melting Onset (Solidus), °C 640
1340
Specific Heat Capacity, J/kg-K 900
490
Thermal Conductivity, W/m-K 210
15
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
25
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.4
4.4
Embodied Energy, MJ/kg 160
63
Embodied Water, L/kg 1200
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.7 to 27
38
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 200
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 15 to 20
18
Strength to Weight: Bending, points 23 to 28
18
Thermal Diffusivity, mm2/s 84
3.9
Thermal Shock Resistance, points 6.7 to 8.6
11

Alloy Composition

Aluminum (Al), % 98.5 to 99.4
0
Carbon (C), % 0
0.3 to 0.5
Chromium (Cr), % 0
24 to 27
Copper (Cu), % 0 to 0.1
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.1
45.4 to 55.7
Magnesium (Mg), % 0.6 to 1.0
0
Manganese (Mn), % 0 to 0.030
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
19 to 22
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.080
1.0 to 2.5
Sulfur (S), % 0
0 to 0.030
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.050
0