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EN 1.4962 Stainless Steel vs. 5019 Aluminum

EN 1.4962 stainless steel belongs to the iron alloys classification, while 5019 aluminum belongs to the aluminum 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 EN 1.4962 stainless steel and the bottom bar is 5019 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 22 to 34
2.2 to 18
Fatigue Strength, MPa 210 to 330
100 to 160
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 420 to 440
170 to 210
Tensile Strength: Ultimate (UTS), MPa 630 to 690
280 to 360
Tensile Strength: Yield (Proof), MPa 260 to 490
120 to 300

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 910
180
Melting Completion (Liquidus), °C 1480
640
Melting Onset (Solidus), °C 1440
540
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 14
130
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
29
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
98

Otherwise Unclassified Properties

Base Metal Price, % relative 23
9.5
Density, g/cm3 8.1
2.7
Embodied Carbon, kg CO2/kg material 4.1
9.0
Embodied Energy, MJ/kg 59
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 170
7.6 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 610
110 to 650
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 21 to 24
29 to 38
Strength to Weight: Bending, points 20 to 21
35 to 42
Thermal Diffusivity, mm2/s 3.7
52
Thermal Shock Resistance, points 14 to 16
13 to 16

Alloy Composition

Aluminum (Al), % 0
91.5 to 95.3
Boron (B), % 0.0015 to 0.0060
0
Carbon (C), % 0.070 to 0.15
0
Chromium (Cr), % 15.5 to 17.5
0 to 0.2
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 62.1 to 69
0 to 0.5
Magnesium (Mg), % 0
4.5 to 5.6
Manganese (Mn), % 0 to 1.5
0.1 to 0.6
Nickel (Ni), % 12.5 to 14.5
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.4 to 0.7
0 to 0.2
Tungsten (W), % 2.5 to 3.0
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15