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S21904 Stainless Steel vs. 7050 Aluminum

S21904 stainless steel belongs to the iron alloys classification, while 7050 aluminum belongs to the aluminum alloys. There are 30 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 7050 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 17 to 51
2.2 to 12
Fatigue Strength, MPa 380 to 550
130 to 210
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 78
26
Shear Strength, MPa 510 to 620
280 to 330
Tensile Strength: Ultimate (UTS), MPa 700 to 1000
490 to 570
Tensile Strength: Yield (Proof), MPa 390 to 910
390 to 500

Thermal Properties

Latent Heat of Fusion, J/g 290
370
Maximum Temperature: Mechanical, °C 980
190
Melting Completion (Liquidus), °C 1400
630
Melting Onset (Solidus), °C 1350
490
Specific Heat Capacity, J/kg-K 480
860
Thermal Conductivity, W/m-K 14
140
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
100

Otherwise Unclassified Properties

Base Metal Price, % relative 15
10
Density, g/cm3 7.7
3.1
Embodied Carbon, kg CO2/kg material 3.0
8.2
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 160
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160 to 310
10 to 55
Resilience: Unit (Modulus of Resilience), kJ/m3 380 to 2070
1110 to 1760
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 25 to 36
45 to 51
Strength to Weight: Bending, points 23 to 29
45 to 50
Thermal Diffusivity, mm2/s 3.8
54
Thermal Shock Resistance, points 15 to 21
21 to 25

Alloy Composition

Aluminum (Al), % 0
87.3 to 92.1
Carbon (C), % 0 to 0.040
0
Chromium (Cr), % 19 to 21.5
0 to 0.040
Copper (Cu), % 0
2.0 to 2.6
Iron (Fe), % 59.5 to 67.4
0 to 0.15
Magnesium (Mg), % 0
1.9 to 2.6
Manganese (Mn), % 8.0 to 10
0 to 0.1
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 0.12
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.060
Zinc (Zn), % 0
5.7 to 6.7
Zirconium (Zr), % 0
0.080 to 0.15
Residuals, % 0
0 to 0.15