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6070 Aluminum vs. EN 1.4982 Stainless Steel

6070 aluminum belongs to the aluminum alloys classification, while EN 1.4982 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 6070 aluminum and the bottom bar is EN 1.4982 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 5.6 to 8.6
28
Fatigue Strength, MPa 95 to 130
420
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 220 to 240
490
Tensile Strength: Ultimate (UTS), MPa 370 to 380
750
Tensile Strength: Yield (Proof), MPa 350
570

Thermal Properties

Latent Heat of Fusion, J/g 410
290
Maximum Temperature: Mechanical, °C 160
860
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 570
1390
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 160
13
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
22
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
4.9
Embodied Energy, MJ/kg 150
71
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 20 to 32
190
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 900
830
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 38
27
Strength to Weight: Bending, points 42 to 43
23
Thermal Diffusivity, mm2/s 65
3.4
Thermal Shock Resistance, points 16 to 17
17

Alloy Composition


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Aluminum (Al), % 94.6 to 98
0
Boron (B), % 0
0.0030 to 0.0090
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0 to 0.1
14 to 16
Copper (Cu), % 0.15 to 0.4
0
Iron (Fe), % 0 to 0.5
61.8 to 69.7
Magnesium (Mg), % 0.5 to 1.2
0
Manganese (Mn), % 0.4 to 1.0
5.5 to 7.0
Molybdenum (Mo), % 0
0.8 to 1.2
Nickel (Ni), % 0
9.0 to 11
Niobium (Nb), % 0
0.75 to 1.3
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 1.0 to 1.7
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Vanadium (V), % 0
0.15 to 0.4
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0