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6105 Aluminum vs. EN 1.4945 Stainless Steel

6105 aluminum belongs to the aluminum alloys classification, while EN 1.4945 stainless steel belongs to the iron alloys. There are 30 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 6105 aluminum and the bottom bar is EN 1.4945 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 9.0 to 16
19 to 34
Fatigue Strength, MPa 95 to 130
230 to 350
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 120 to 170
430 to 460
Tensile Strength: Ultimate (UTS), MPa 190 to 280
640 to 740
Tensile Strength: Yield (Proof), MPa 120 to 270
290 to 550

Thermal Properties

Latent Heat of Fusion, J/g 410
290
Maximum Temperature: Mechanical, °C 160
920
Melting Completion (Liquidus), °C 650
1490
Melting Onset (Solidus), °C 600
1440
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 180 to 190
14
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 46 to 50
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 150 to 170
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.7
8.1
Embodied Carbon, kg CO2/kg material 8.3
5.0
Embodied Energy, MJ/kg 150
73
Embodied Water, L/kg 1180
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25 to 27
130 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 550
210 to 760
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 20 to 29
22 to 25
Strength to Weight: Bending, points 28 to 35
20 to 22
Thermal Diffusivity, mm2/s 72 to 79
3.7
Thermal Shock Resistance, points 8.6 to 12
14 to 16

Alloy Composition


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Aluminum (Al), % 97.2 to 99
0
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0 to 0.1
15.5 to 17.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.35
57.9 to 65.7
Magnesium (Mg), % 0.45 to 0.8
0
Manganese (Mn), % 0 to 0.1
0 to 1.5
Nickel (Ni), % 0
15.5 to 17.5
Niobium (Nb), % 0
0.4 to 1.2
Nitrogen (N), % 0
0.060 to 0.14
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0.6 to 1.0
0.3 to 0.6
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
2.5 to 3.5
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0