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S21904 Stainless Steel vs. 535.0 Aluminum

S21904 stainless steel belongs to the iron alloys classification, while 535.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 S21904 stainless steel and the bottom bar is 535.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 300
70
Elastic (Young's, Tensile) Modulus, GPa 200
67
Elongation at Break, % 17 to 51
10
Fatigue Strength, MPa 380 to 550
70
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
25
Shear Strength, MPa 510 to 620
190
Tensile Strength: Ultimate (UTS), MPa 700 to 1000
270
Tensile Strength: Yield (Proof), MPa 390 to 910
140

Thermal Properties

Latent Heat of Fusion, J/g 290
390
Maximum Temperature: Mechanical, °C 980
170
Melting Completion (Liquidus), °C 1400
630
Melting Onset (Solidus), °C 1350
570
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 14
100
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
23
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
79

Otherwise Unclassified Properties

Base Metal Price, % relative 15
9.5
Density, g/cm3 7.7
2.6
Embodied Carbon, kg CO2/kg material 3.0
9.4
Embodied Energy, MJ/kg 43
160
Embodied Water, L/kg 160
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160 to 310
24
Resilience: Unit (Modulus of Resilience), kJ/m3 380 to 2070
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 25 to 36
28
Strength to Weight: Bending, points 23 to 29
35
Thermal Diffusivity, mm2/s 3.8
42
Thermal Shock Resistance, points 15 to 21
12

Alloy Composition


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Aluminum (Al), % 0
91.5 to 93.6
Beryllium (Be), % 0
0.0030 to 0.0070
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 19 to 21.5
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 59.5 to 67.4
0 to 0.15
Magnesium (Mg), % 0
6.2 to 7.5
Manganese (Mn), % 8.0 to 10
0.1 to 0.25
Nickel (Ni), % 5.5 to 7.5
0
Nitrogen (N), % 0.15 to 0.4
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.15
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0.1 to 0.25
Residuals, % 0
0 to 0.15