MakeItFrom.com
Menu (ESC)

EN 1.7386 Steel vs. 5070 Aluminum

EN 1.7386 steel belongs to the iron alloys classification, while 5070 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 1.7386 steel and the bottom bar is 5070 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 18 to 21
20
Fatigue Strength, MPa 170 to 290
150
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 340 to 410
190
Tensile Strength: Ultimate (UTS), MPa 550 to 670
300
Tensile Strength: Yield (Proof), MPa 240 to 440
140

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Maximum Temperature: Mechanical, °C 600
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1410
550
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 26
130
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.0
31
Electrical Conductivity: Equal Weight (Specific), % IACS 10
100

Otherwise Unclassified Properties

Base Metal Price, % relative 6.5
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.0
8.8
Embodied Energy, MJ/kg 28
150
Embodied Water, L/kg 88
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 110
51
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 490
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 20 to 24
31
Strength to Weight: Bending, points 19 to 22
37
Thermal Diffusivity, mm2/s 6.9
53
Thermal Shock Resistance, points 15 to 18
14

Alloy Composition

Aluminum (Al), % 0 to 0.040
92.4 to 95.7
Carbon (C), % 0.080 to 0.15
0
Chromium (Cr), % 8.0 to 10
0 to 0.3
Copper (Cu), % 0 to 0.3
0 to 0.25
Iron (Fe), % 86.8 to 90.5
0 to 0.4
Magnesium (Mg), % 0
3.5 to 4.5
Manganese (Mn), % 0.3 to 0.6
0.4 to 0.8
Molybdenum (Mo), % 0.9 to 1.1
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.25 to 1.0
0 to 0.25
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0.4 to 0.8
Residuals, % 0
0 to 0.15