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EN 1.4872 Stainless Steel vs. 6005 Aluminum

EN 1.4872 stainless steel belongs to the iron alloys classification, while 6005 aluminum belongs to the aluminum alloys. There are 31 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 EN 1.4872 stainless steel and the bottom bar is 6005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 270
90 to 95
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 28
9.5 to 17
Fatigue Strength, MPa 410
55 to 95
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 620
120 to 210
Tensile Strength: Ultimate (UTS), MPa 950
190 to 310
Tensile Strength: Yield (Proof), MPa 560
100 to 280

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 1150
160
Melting Completion (Liquidus), °C 1390
650
Melting Onset (Solidus), °C 1340
610
Specific Heat Capacity, J/kg-K 490
900
Thermal Conductivity, W/m-K 15
180 to 200
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
54
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
180

Otherwise Unclassified Properties

Base Metal Price, % relative 17
9.5
Density, g/cm3 7.6
2.7
Embodied Carbon, kg CO2/kg material 3.3
8.3
Embodied Energy, MJ/kg 47
150
Embodied Water, L/kg 180
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 230
27 to 36
Resilience: Unit (Modulus of Resilience), kJ/m3 780
77 to 550
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 26
51
Strength to Weight: Axial, points 35
20 to 32
Strength to Weight: Bending, points 28
28 to 38
Thermal Diffusivity, mm2/s 3.9
74 to 83
Thermal Shock Resistance, points 21
8.6 to 14

Alloy Composition

Aluminum (Al), % 0
97.5 to 99
Carbon (C), % 0.2 to 0.3
0
Chromium (Cr), % 24 to 26
0 to 0.1
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 54.2 to 61.6
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 8.0 to 10
0 to 0.1
Nickel (Ni), % 6.0 to 8.0
0
Nitrogen (N), % 0.2 to 0.4
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0.6 to 0.9
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15