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S15500 Stainless Steel vs. 2117 Aluminum

S15500 stainless steel belongs to the iron alloys classification, while 2117 aluminum belongs to the aluminum alloys. There are 31 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 S15500 stainless steel and the bottom bar is 2117 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 290 to 430
70
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 6.8 to 16
26
Fatigue Strength, MPa 350 to 650
95
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 540 to 870
200
Tensile Strength: Ultimate (UTS), MPa 890 to 1490
300
Tensile Strength: Yield (Proof), MPa 590 to 1310
170

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 820
220
Melting Completion (Liquidus), °C 1430
650
Melting Onset (Solidus), °C 1380
550
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 17
150
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 13
10
Density, g/cm3 7.8
3.0
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
64
Resilience: Unit (Modulus of Resilience), kJ/m3 890 to 4460
190
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 32 to 53
28
Strength to Weight: Bending, points 26 to 37
33
Thermal Diffusivity, mm2/s 4.6
59
Thermal Shock Resistance, points 30 to 50
12

Alloy Composition

Aluminum (Al), % 0
91 to 97.6
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 14 to 15.5
0 to 0.1
Copper (Cu), % 2.5 to 4.5
2.2 to 4.5
Iron (Fe), % 71.9 to 79.9
0 to 0.7
Magnesium (Mg), % 0
0.2 to 1.0
Manganese (Mn), % 0 to 1.0
0.4 to 1.0
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
0.2 to 0.8
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15