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1070 Aluminum vs. EN 1.4560 Stainless Steel

1070 aluminum belongs to the aluminum alloys classification, while EN 1.4560 stainless steel belongs to the iron 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 1070 aluminum and the bottom bar is EN 1.4560 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 4.5 to 39
50
Fatigue Strength, MPa 22 to 49
190
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 48 to 79
390
Tensile Strength: Ultimate (UTS), MPa 73 to 140
550
Tensile Strength: Yield (Proof), MPa 17 to 120
190

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 170
940
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 640
1370
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 230
15
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 200
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
15
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
3.0
Embodied Energy, MJ/kg 160
42
Embodied Water, L/kg 1200
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.8 to 21
220
Resilience: Unit (Modulus of Resilience), kJ/m3 2.1 to 110
92
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 7.5 to 14
20
Strength to Weight: Bending, points 14 to 22
19
Thermal Diffusivity, mm2/s 94
4.0
Thermal Shock Resistance, points 3.3 to 6.1
12

Alloy Composition

Aluminum (Al), % 99.7 to 100
0
Carbon (C), % 0
0 to 0.035
Chromium (Cr), % 0
18 to 19
Copper (Cu), % 0 to 0.040
1.5 to 2.0
Iron (Fe), % 0 to 0.25
66.8 to 71
Magnesium (Mg), % 0 to 0.030
0
Manganese (Mn), % 0 to 0.030
1.5 to 2.0
Nickel (Ni), % 0
8.0 to 9.0
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.030
0
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.040
0
Residuals, % 0 to 0.030
0