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EN 1.4606 Stainless Steel vs. 705.0 Aluminum

EN 1.4606 stainless steel belongs to the iron alloys classification, while 705.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 1.4606 stainless steel and the bottom bar is 705.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 23 to 39
8.4 to 10
Fatigue Strength, MPa 240 to 420
63 to 98
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
26
Tensile Strength: Ultimate (UTS), MPa 600 to 1020
240 to 260
Tensile Strength: Yield (Proof), MPa 280 to 630
130

Thermal Properties

Latent Heat of Fusion, J/g 300
390
Maximum Temperature: Mechanical, °C 910
180
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
610
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
34
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
110

Otherwise Unclassified Properties

Base Metal Price, % relative 26
9.5
Density, g/cm3 7.9
2.8
Embodied Carbon, kg CO2/kg material 6.0
8.4
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190 to 200
18 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 1010
120 to 130
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
49
Strength to Weight: Axial, points 21 to 36
24 to 26
Strength to Weight: Bending, points 20 to 28
31 to 32
Thermal Diffusivity, mm2/s 3.7
55
Thermal Shock Resistance, points 21 to 35
11

Alloy Composition

Aluminum (Al), % 0 to 0.35
92.3 to 98.6
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13 to 16
0 to 0.4
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 49.2 to 59
0 to 0.8
Magnesium (Mg), % 0
1.4 to 1.8
Manganese (Mn), % 1.0 to 2.0
0 to 0.6
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 1.9 to 2.3
0 to 0.25
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
0 to 3.3
Residuals, % 0
0 to 0.15