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EN 1.4662 Stainless Steel vs. 7129 Aluminum

EN 1.4662 stainless steel belongs to the iron alloys classification, while 7129 Aluminum belongs to the aluminum alloys. There are 30 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 EN 1.4662 stainless steel and the bottom bar is 7129 Aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 28
9.0 to 9.1
Fatigue Strength, MPa 430 to 450
150 to 190
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 520 to 540
250 to 260
Tensile Strength: Ultimate (UTS), MPa 810 to 830
430
Tensile Strength: Yield (Proof), MPa 580 to 620
380 to 390

Thermal Properties

Latent Heat of Fusion, J/g 290
380
Maximum Temperature: Mechanical, °C 1090
180
Melting Completion (Liquidus), °C 1430
630
Melting Onset (Solidus), °C 1380
510
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 15
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
120

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Density, g/cm3 7.7
2.9
Embodied Carbon, kg CO2/kg material 3.2
8.3
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 170
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
37 to 38
Resilience: Unit (Modulus of Resilience), kJ/m3 840 to 940
1050 to 1090
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 29 to 30
41
Strength to Weight: Bending, points 25
43 to 44
Thermal Diffusivity, mm2/s 3.9
58
Thermal Shock Resistance, points 22
19

Alloy Composition

Aluminum (Al), % 0
91 to 94
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 23 to 25
0 to 0.1
Copper (Cu), % 0.1 to 0.8
0.5 to 0.9
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 62.6 to 70.2
0 to 0.3
Magnesium (Mg), % 0
1.3 to 2.0
Manganese (Mn), % 2.5 to 4.0
0 to 0.1
Molybdenum (Mo), % 1.0 to 2.0
0
Nickel (Ni), % 3.0 to 4.5
0
Nitrogen (N), % 0.2 to 0.3
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.7
0 to 0.15
Sulfur (S), % 0 to 0.0050
0
Titanium (Ti), % 0
0 to 0.050
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
4.2 to 5.2
Residuals, % 0
0 to 0.15