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EN 1.4980 Stainless Steel vs. 6005 Aluminum

EN 1.4980 stainless steel belongs to the iron alloys classification, while 6005 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 1.4980 stainless steel and the bottom bar is 6005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 17
9.5 to 17
Fatigue Strength, MPa 410
55 to 95
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 630
120 to 210
Tensile Strength: Ultimate (UTS), MPa 1030
190 to 310
Tensile Strength: Yield (Proof), MPa 680
100 to 280

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 920
160
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1380
610
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 13
180 to 200
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
54
Electrical Conductivity: Equal Weight (Specific), % IACS 2.1
180

Otherwise Unclassified Properties

Base Metal Price, % relative 26
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 6.0
8.3
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150
27 to 36
Resilience: Unit (Modulus of Resilience), kJ/m3 1180
77 to 550
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 36
20 to 32
Strength to Weight: Bending, points 28
28 to 38
Thermal Diffusivity, mm2/s 3.5
74 to 83
Thermal Shock Resistance, points 22
8.6 to 14

Alloy Composition

Aluminum (Al), % 0 to 0.35
97.5 to 99
Boron (B), % 0.0030 to 0.010
0
Carbon (C), % 0.030 to 0.080
0
Chromium (Cr), % 13.5 to 16
0 to 0.1
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 49.2 to 58.5
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 1.0 to 2.0
0 to 0.1
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
0.6 to 0.9
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0 to 0.1
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15