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SAE-AISI 1151 Steel vs. 850.0 Aluminum

SAE-AISI 1151 steel belongs to the iron alloys classification, while 850.0 aluminum belongs to the aluminum alloys. There are 31 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 1151 steel and the bottom bar is 850.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 220
45
Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 11 to 17
7.9
Fatigue Strength, MPa 260 to 410
59
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 430 to 480
100
Tensile Strength: Ultimate (UTS), MPa 710 to 800
140
Tensile Strength: Yield (Proof), MPa 390 to 660
76

Thermal Properties

Latent Heat of Fusion, J/g 250
380
Maximum Temperature: Mechanical, °C 400
190
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
370
Specific Heat Capacity, J/kg-K 470
850
Thermal Conductivity, W/m-K 51
180
Thermal Expansion, µm/m-K 12
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
47
Electrical Conductivity: Equal Weight (Specific), % IACS 12
140

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
14
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 1.4
8.5
Embodied Energy, MJ/kg 18
160
Embodied Water, L/kg 46
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 86 to 100
9.1
Resilience: Unit (Modulus of Resilience), kJ/m3 400 to 1170
42
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 24
44
Strength to Weight: Axial, points 25 to 28
12
Strength to Weight: Bending, points 22 to 24
19
Thermal Diffusivity, mm2/s 14
69
Thermal Shock Resistance, points 22 to 25
6.1

Alloy Composition


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Aluminum (Al), % 0
88.3 to 93.1
Carbon (C), % 0.48 to 0.55
0
Copper (Cu), % 0
0.7 to 1.3
Iron (Fe), % 98.3 to 98.7
0 to 0.7
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.7 to 1.0
0 to 0.1
Nickel (Ni), % 0
0.7 to 1.3
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0 to 0.7
Sulfur (S), % 0.080 to 0.13
0
Tin (Sn), % 0
5.5 to 7.0
Titanium (Ti), % 0
0 to 0.2
Residuals, % 0
0 to 0.3