MakeItFrom.com
Menu (ESC)

5019 Aluminum vs. S32053 Stainless Steel

5019 aluminum belongs to the aluminum alloys classification, while S32053 stainless steel belongs to the iron alloys. There are 30 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 5019 aluminum and the bottom bar is S32053 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 2.2 to 18
46
Fatigue Strength, MPa 100 to 160
310
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
80
Shear Strength, MPa 170 to 210
510
Tensile Strength: Ultimate (UTS), MPa 280 to 360
730
Tensile Strength: Yield (Proof), MPa 120 to 300
330

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 540
1400
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
13
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 98
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
33
Density, g/cm3 2.7
8.1
Embodied Carbon, kg CO2/kg material 9.0
6.1
Embodied Energy, MJ/kg 150
83
Embodied Water, L/kg 1180
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.6 to 40
270
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 650
270
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 29 to 38
25
Strength to Weight: Bending, points 35 to 42
22
Thermal Diffusivity, mm2/s 52
3.3
Thermal Shock Resistance, points 13 to 16
16

Alloy Composition

Aluminum (Al), % 91.5 to 95.3
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.2
22 to 24
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.5
41.7 to 48.8
Magnesium (Mg), % 4.5 to 5.6
0
Manganese (Mn), % 0.1 to 0.6
0 to 1.0
Molybdenum (Mo), % 0
5.0 to 6.0
Nickel (Ni), % 0
24 to 26
Nitrogen (N), % 0
0.17 to 0.22
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0