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EN 1.4872 Stainless Steel vs. 7049A Aluminum

EN 1.4872 stainless steel belongs to the iron alloys classification, while 7049A 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 EN 1.4872 stainless steel and the bottom bar is 7049A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 28
5.0 to 5.7
Fatigue Strength, MPa 410
180
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 79
27
Shear Strength, MPa 620
340 to 350
Tensile Strength: Ultimate (UTS), MPa 950
580 to 590
Tensile Strength: Yield (Proof), MPa 560
500 to 530

Thermal Properties

Latent Heat of Fusion, J/g 300
370
Maximum Temperature: Mechanical, °C 1150
200
Melting Completion (Liquidus), °C 1390
640
Melting Onset (Solidus), °C 1340
430
Specific Heat Capacity, J/kg-K 490
850
Thermal Conductivity, W/m-K 15
130
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
40
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
120

Otherwise Unclassified Properties

Base Metal Price, % relative 17
10
Density, g/cm3 7.6
3.1
Embodied Carbon, kg CO2/kg material 3.3
8.2
Embodied Energy, MJ/kg 47
150
Embodied Water, L/kg 180
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 230
28 to 32
Resilience: Unit (Modulus of Resilience), kJ/m3 780
1800 to 1990
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 26
44
Strength to Weight: Axial, points 35
52 to 53
Strength to Weight: Bending, points 28
50 to 51
Thermal Diffusivity, mm2/s 3.9
50
Thermal Shock Resistance, points 21
25

Alloy Composition

Aluminum (Al), % 0
84.6 to 89.5
Carbon (C), % 0.2 to 0.3
0
Chromium (Cr), % 24 to 26
0.050 to 0.25
Copper (Cu), % 0
1.2 to 1.9
Iron (Fe), % 54.2 to 61.6
0 to 0.5
Magnesium (Mg), % 0
2.1 to 3.1
Manganese (Mn), % 8.0 to 10
0 to 0.5
Nickel (Ni), % 6.0 to 8.0
0
Nitrogen (N), % 0.2 to 0.4
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
7.2 to 8.4
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15