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7050 Aluminum vs. EN 1.4923 Stainless Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.4923 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 7050 aluminum and the bottom bar is EN 1.4923 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
12 to 21
Fatigue Strength, MPa 130 to 210
300 to 440
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 280 to 330
540 to 590
Tensile Strength: Ultimate (UTS), MPa 490 to 570
870 to 980
Tensile Strength: Yield (Proof), MPa 390 to 500
470 to 780

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Maximum Temperature: Mechanical, °C 190
740
Melting Completion (Liquidus), °C 630
1450
Melting Onset (Solidus), °C 490
1410
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 140
24
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
8.0
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.9
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1120
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
570 to 1580
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 45 to 51
31 to 35
Strength to Weight: Bending, points 45 to 50
26 to 28
Thermal Diffusivity, mm2/s 54
6.5
Thermal Shock Resistance, points 21 to 25
30 to 34

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0.18 to 0.24
Chromium (Cr), % 0 to 0.040
11 to 12.5
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
83.5 to 87.1
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0.4 to 0.9
Molybdenum (Mo), % 0
0.8 to 1.2
Nickel (Ni), % 0
0.3 to 0.8
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.060
0
Vanadium (V), % 0
0.25 to 0.35
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0

Comparable Variants