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S17400 Stainless Steel vs. 2117 Aluminum

S17400 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 S17400 stainless steel and the bottom bar is 2117 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 280 to 440
70
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 11 to 21
26
Fatigue Strength, MPa 380 to 670
95
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 570 to 830
200
Tensile Strength: Ultimate (UTS), MPa 910 to 1390
300
Tensile Strength: Yield (Proof), MPa 580 to 1250
170

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 850
220
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1400
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 2.3
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
120

Otherwise Unclassified Properties

Base Metal Price, % relative 14
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 140 to 160
64
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4060
190
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 32 to 49
28
Strength to Weight: Bending, points 27 to 35
33
Thermal Diffusivity, mm2/s 4.5
59
Thermal Shock Resistance, points 30 to 46
12

Alloy Composition


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Aluminum (Al), % 0
91 to 97.6
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0 to 0.1
Copper (Cu), % 3.0 to 5.0
2.2 to 4.5
Iron (Fe), % 70.4 to 78.9
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), % 3.0 to 5.0
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