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S17600 Stainless Steel vs. B535.0 Aluminum

S17600 stainless steel belongs to the iron alloys classification, while B535.0 aluminum belongs to the aluminum 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 S17600 stainless steel and the bottom bar is B535.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 270 to 410
65
Elastic (Young's, Tensile) Modulus, GPa 200
66
Elongation at Break, % 8.6 to 11
10
Fatigue Strength, MPa 300 to 680
62
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
25
Shear Strength, MPa 560 to 880
210
Tensile Strength: Ultimate (UTS), MPa 940 to 1490
260
Tensile Strength: Yield (Proof), MPa 580 to 1310
130

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 890
170
Melting Completion (Liquidus), °C 1430
630
Melting Onset (Solidus), °C 1390
550
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 15
96
Thermal Expansion, µm/m-K 11
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
24
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
82

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.8
2.6
Embodied Carbon, kg CO2/kg material 2.9
9.4
Embodied Energy, MJ/kg 42
160
Embodied Water, L/kg 130
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 70 to 150
22
Resilience: Unit (Modulus of Resilience), kJ/m3 850 to 4390
130
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 34 to 54
28
Strength to Weight: Bending, points 28 to 37
35
Thermal Diffusivity, mm2/s 4.1
40
Thermal Shock Resistance, points 31 to 50
11

Alloy Composition

Aluminum (Al), % 0 to 0.4
91.7 to 93.4
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 16 to 17.5
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 71.3 to 77.6
0 to 0.15
Magnesium (Mg), % 0
6.5 to 7.5
Manganese (Mn), % 0 to 1.0
0 to 0.050
Nickel (Ni), % 6.0 to 7.5
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.15
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0.4 to 1.2
0.1 to 0.25
Residuals, % 0
0 to 0.15