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AISI 422 Stainless Steel vs. 7475 Aluminum

AISI 422 stainless steel belongs to the iron alloys classification, while 7475 aluminum belongs to the aluminum alloys. There are 30 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 AISI 422 stainless steel and the bottom bar is 7475 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 15 to 17
10 to 12
Fatigue Strength, MPa 410 to 500
190 to 210
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
26
Shear Strength, MPa 560 to 660
320 to 350
Tensile Strength: Ultimate (UTS), MPa 910 to 1080
530 to 590
Tensile Strength: Yield (Proof), MPa 670 to 870
440 to 520

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 650
180
Melting Completion (Liquidus), °C 1480
640
Melting Onset (Solidus), °C 1470
480
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 24
140 to 160
Thermal Expansion, µm/m-K 10
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.7
33 to 42
Electrical Conductivity: Equal Weight (Specific), % IACS 5.3
98 to 120

Otherwise Unclassified Properties

Base Metal Price, % relative 11
10
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 3.1
8.2
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 150
53 to 68
Resilience: Unit (Modulus of Resilience), kJ/m3 1140 to 1910
1390 to 1920
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 32 to 38
49 to 55
Strength to Weight: Bending, points 26 to 30
48 to 52
Thermal Diffusivity, mm2/s 6.4
53 to 63
Thermal Shock Resistance, points 33 to 39
23 to 26

Alloy Composition

Aluminum (Al), % 0
88.6 to 91.6
Carbon (C), % 0.2 to 0.25
0
Chromium (Cr), % 11 to 12.5
0.18 to 0.25
Copper (Cu), % 0
1.2 to 1.9
Iron (Fe), % 81.9 to 85.8
0 to 0.12
Magnesium (Mg), % 0
1.9 to 2.6
Manganese (Mn), % 0.5 to 1.0
0 to 0.060
Molybdenum (Mo), % 0.9 to 1.3
0
Nickel (Ni), % 0.5 to 1.0
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.1
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.060
Tungsten (W), % 0.9 to 1.3
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
5.1 to 6.2
Residuals, % 0
0 to 0.15