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2219 Aluminum vs. EN 1.4962 Stainless Steel

2219 aluminum belongs to the aluminum alloys classification, while EN 1.4962 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 2219 aluminum and the bottom bar is EN 1.4962 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 2.2 to 20
22 to 34
Fatigue Strength, MPa 90 to 130
210 to 330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
77
Shear Strength, MPa 110 to 280
420 to 440
Tensile Strength: Ultimate (UTS), MPa 180 to 480
630 to 690
Tensile Strength: Yield (Proof), MPa 88 to 390
260 to 490

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 230
910
Melting Completion (Liquidus), °C 640
1480
Melting Onset (Solidus), °C 540
1440
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 110 to 170
14
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28 to 44
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 81 to 130
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 11
23
Density, g/cm3 3.1
8.1
Embodied Carbon, kg CO2/kg material 8.2
4.1
Embodied Energy, MJ/kg 150
59
Embodied Water, L/kg 1130
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.6 to 60
140 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 54 to 1060
170 to 610
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 44
24
Strength to Weight: Axial, points 16 to 43
21 to 24
Strength to Weight: Bending, points 23 to 44
20 to 21
Thermal Diffusivity, mm2/s 42 to 63
3.7
Thermal Shock Resistance, points 8.2 to 22
14 to 16

Alloy Composition


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Aluminum (Al), % 91.5 to 93.8
0
Boron (B), % 0
0.0015 to 0.0060
Carbon (C), % 0
0.070 to 0.15
Chromium (Cr), % 0
15.5 to 17.5
Copper (Cu), % 5.8 to 6.8
0
Iron (Fe), % 0 to 0.3
62.1 to 69
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0.2 to 0.4
0 to 1.5
Nickel (Ni), % 0
12.5 to 14.5
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0.020 to 0.1
0.4 to 0.7
Tungsten (W), % 0
2.5 to 3.0
Vanadium (V), % 0.050 to 0.15
0
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0.1 to 0.25
0
Residuals, % 0 to 0.15
0