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EN 1.4872 Stainless Steel vs. 1060 Aluminum

EN 1.4872 stainless steel belongs to the iron alloys classification, while 1060 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 1060 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 28
1.1 to 30
Fatigue Strength, MPa 410
15 to 50
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 620
42 to 75
Tensile Strength: Ultimate (UTS), MPa 950
67 to 130
Tensile Strength: Yield (Proof), MPa 560
17 to 110

Thermal Properties

Latent Heat of Fusion, J/g 300
400
Maximum Temperature: Mechanical, °C 1150
170
Melting Completion (Liquidus), °C 1390
660
Melting Onset (Solidus), °C 1340
650
Specific Heat Capacity, J/kg-K 490
900
Thermal Conductivity, W/m-K 15
230
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
62
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
210

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
160
Embodied Water, L/kg 180
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 230
0.57 to 37
Resilience: Unit (Modulus of Resilience), kJ/m3 780
2.1 to 89
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 26
50
Strength to Weight: Axial, points 35
6.9 to 13
Strength to Weight: Bending, points 28
14 to 21
Thermal Diffusivity, mm2/s 3.9
96
Thermal Shock Resistance, points 21
3.0 to 5.6

Alloy Composition

Aluminum (Al), % 0
99.6 to 100
Carbon (C), % 0.2 to 0.3
0
Chromium (Cr), % 24 to 26
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 54.2 to 61.6
0 to 0.35
Magnesium (Mg), % 0
0 to 0.030
Manganese (Mn), % 8.0 to 10
0 to 0.030
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 to 0.25
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.030
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050