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S21904 Stainless Steel vs. 1050A Aluminum

S21904 stainless steel belongs to the iron alloys classification, while 1050A aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 1050A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 300
20 to 45
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 17 to 51
1.1 to 33
Fatigue Strength, MPa 380 to 550
22 to 55
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 510 to 620
44 to 97
Tensile Strength: Ultimate (UTS), MPa 700 to 1000
68 to 170
Tensile Strength: Yield (Proof), MPa 390 to 910
22 to 150

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 980
170
Melting Completion (Liquidus), °C 1400
660
Melting Onset (Solidus), °C 1350
650
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 14
230
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
59
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
200

Otherwise Unclassified Properties

Base Metal Price, % relative 15
9.0
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 3.0
8.2
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 160
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160 to 310
1.9 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 380 to 2070
3.7 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 25 to 36
6.9 to 18
Strength to Weight: Bending, points 23 to 29
14 to 25
Thermal Diffusivity, mm2/s 3.8
94
Thermal Shock Resistance, points 15 to 21
3.0 to 7.6

Alloy Composition

Aluminum (Al), % 0
99.5 to 100
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 0.4
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 8.0 to 10
0 to 0.050
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 0.25
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.070

Comparable Variants