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2117 Aluminum vs. S17600 Stainless Steel

2117 aluminum belongs to the aluminum alloys classification, while S17600 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 2117 aluminum and the bottom bar is S17600 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 70
270 to 410
Elastic (Young's, Tensile) Modulus, GPa 71
200
Elongation at Break, % 26
8.6 to 11
Fatigue Strength, MPa 95
300 to 680
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 200
560 to 880
Tensile Strength: Ultimate (UTS), MPa 300
940 to 1490
Tensile Strength: Yield (Proof), MPa 170
580 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 220
890
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 550
1390
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 150
15
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.9
Embodied Energy, MJ/kg 150
42
Embodied Water, L/kg 1150
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 64
70 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 190
850 to 4390
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 28
34 to 54
Strength to Weight: Bending, points 33
28 to 37
Thermal Diffusivity, mm2/s 59
4.1
Thermal Shock Resistance, points 12
31 to 50

Alloy Composition

Aluminum (Al), % 91 to 97.6
0 to 0.4
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.1
16 to 17.5
Copper (Cu), % 2.2 to 4.5
0
Iron (Fe), % 0 to 0.7
71.3 to 77.6
Magnesium (Mg), % 0.2 to 1.0
0
Manganese (Mn), % 0.4 to 1.0
0 to 1.0
Nickel (Ni), % 0
6.0 to 7.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.2 to 0.8
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0.4 to 1.2
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0