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SAE-AISI 1552 Steel vs. 358.0 Aluminum

SAE-AISI 1552 steel belongs to the iron alloys classification, while 358.0 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 SAE-AISI 1552 steel and the bottom bar is 358.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 11 to 14
3.5 to 6.0
Fatigue Strength, MPa 290 to 400
100 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
27
Shear Strength, MPa 460 to 510
300 to 320
Tensile Strength: Ultimate (UTS), MPa 760 to 840
350 to 370
Tensile Strength: Yield (Proof), MPa 460 to 650
290 to 320

Thermal Properties

Latent Heat of Fusion, J/g 250
520
Maximum Temperature: Mechanical, °C 400
170
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1420
560
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 51
150
Thermal Expansion, µm/m-K 11
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
36
Electrical Conductivity: Equal Weight (Specific), % IACS 12
130

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
19
Density, g/cm3 7.8
2.6
Embodied Carbon, kg CO2/kg material 1.4
8.7
Embodied Energy, MJ/kg 19
160
Embodied Water, L/kg 47
1090

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 81 to 98
12 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 1130
590 to 710
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
53
Strength to Weight: Axial, points 27 to 30
37 to 39
Strength to Weight: Bending, points 24 to 25
42 to 44
Thermal Diffusivity, mm2/s 14
63
Thermal Shock Resistance, points 26 to 29
16 to 17

Alloy Composition


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Aluminum (Al), % 0
89.1 to 91.8
Beryllium (Be), % 0
0.1 to 0.3
Carbon (C), % 0.47 to 0.55
0
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 97.9 to 98.3
0 to 0.3
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 1.2 to 1.5
0 to 0.2
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
7.6 to 8.6
Sulfur (S), % 0 to 0.050
0
Titanium (Ti), % 0
0.1 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15