MakeItFrom.com
Menu (ESC)

S15500 Stainless Steel vs. 2219 Aluminum

S15500 stainless steel belongs to the iron alloys classification, while 2219 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 S15500 stainless steel and the bottom bar is 2219 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 6.8 to 16
2.2 to 20
Fatigue Strength, MPa 350 to 650
90 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 540 to 870
110 to 280
Tensile Strength: Ultimate (UTS), MPa 890 to 1490
180 to 480
Tensile Strength: Yield (Proof), MPa 590 to 1310
88 to 390

Thermal Properties

Latent Heat of Fusion, J/g 280
390
Maximum Temperature: Mechanical, °C 820
230
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
540
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 17
110 to 170
Thermal Expansion, µm/m-K 11
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
28 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
81 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 13
11
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
9.6 to 60
Resilience: Unit (Modulus of Resilience), kJ/m3 890 to 4460
54 to 1060
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
44
Strength to Weight: Axial, points 32 to 53
16 to 43
Strength to Weight: Bending, points 26 to 37
23 to 44
Thermal Diffusivity, mm2/s 4.6
42 to 63
Thermal Shock Resistance, points 30 to 50
8.2 to 22

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0
91.5 to 93.8
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 14 to 15.5
0
Copper (Cu), % 2.5 to 4.5
5.8 to 6.8
Iron (Fe), % 71.9 to 79.9
0 to 0.3
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 0 to 1.0
0.2 to 0.4
Nickel (Ni), % 3.5 to 5.5
0
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0.020 to 0.1
Vanadium (V), % 0
0.050 to 0.15
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0
0.1 to 0.25
Residuals, % 0
0 to 0.15