MakeItFrom.com
Menu (ESC)

242.0 Aluminum vs. S21900 Stainless Steel

242.0 aluminum belongs to the aluminum alloys classification, while S21900 stainless steel belongs to the iron 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 242.0 aluminum and the bottom bar is S21900 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 70 to 110
220
Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 0.5 to 1.5
50
Fatigue Strength, MPa 55 to 110
380
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Shear Strength, MPa 150 to 240
510
Tensile Strength: Ultimate (UTS), MPa 180 to 290
710
Tensile Strength: Yield (Proof), MPa 120 to 220
390

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Mechanical, °C 210
980
Melting Completion (Liquidus), °C 640
1400
Melting Onset (Solidus), °C 530
1350
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 130 to 170
14
Thermal Expansion, µm/m-K 22
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
15
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 8.3
3.0
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1130
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
300
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
380
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 16 to 26
26
Strength to Weight: Bending, points 23 to 32
23
Thermal Diffusivity, mm2/s 50 to 62
3.8
Thermal Shock Resistance, points 8.0 to 13
15

Alloy Composition

Aluminum (Al), % 88.4 to 93.6
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.25
19 to 21.5
Copper (Cu), % 3.5 to 4.5
0
Iron (Fe), % 0 to 1.0
59.4 to 67.4
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
8.0 to 10
Nickel (Ni), % 1.7 to 2.3
5.5 to 7.5
Nitrogen (N), % 0
0.15 to 0.4
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.7
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0