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A206.0 Aluminum vs. EN 1.4905 Stainless Steel

A206.0 aluminum belongs to the aluminum alloys classification, while EN 1.4905 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 A206.0 aluminum and the bottom bar is EN 1.4905 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 4.2 to 10
19
Fatigue Strength, MPa 90 to 180
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 260
460
Tensile Strength: Ultimate (UTS), MPa 390 to 440
740
Tensile Strength: Yield (Proof), MPa 250 to 380
510

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 170
660
Melting Completion (Liquidus), °C 670
1480
Melting Onset (Solidus), °C 550
1440
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
26
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
3.7
Electrical Conductivity: Equal Weight (Specific), % IACS 90
4.2

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 3.0
7.9
Embodied Carbon, kg CO2/kg material 8.0
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1150
90

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 37
130
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1000
680
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
24
Strength to Weight: Axial, points 36 to 41
26
Strength to Weight: Bending, points 39 to 43
23
Thermal Diffusivity, mm2/s 48
7.0
Thermal Shock Resistance, points 17 to 19
25

Alloy Composition

Aluminum (Al), % 93.9 to 95.7
0 to 0.040
Boron (B), % 0
0.00050 to 0.0050
Carbon (C), % 0
0.090 to 0.13
Chromium (Cr), % 0
8.5 to 9.5
Copper (Cu), % 4.2 to 5.0
0
Iron (Fe), % 0 to 0.1
86.2 to 88.8
Magnesium (Mg), % 0 to 0.15
0
Manganese (Mn), % 0 to 0.2
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.050
0.1 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.050 to 0.090
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.050
0.1 to 0.5
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.15 to 0.3
0
Tungsten (W), % 0
0.9 to 1.1
Vanadium (V), % 0
0.18 to 0.25
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0