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1350 Aluminum vs. ASTM A387 Grade 22L Class 1

1350 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 22L class 1 belongs to the iron 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 1350 aluminum and the bottom bar is ASTM A387 grade 22L class 1.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 20 to 45
150
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.4 to 30
20
Fatigue Strength, MPa 24 to 50
160
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 44 to 110
310
Tensile Strength: Ultimate (UTS), MPa 68 to 190
500
Tensile Strength: Yield (Proof), MPa 25 to 170
230

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 170
460
Melting Completion (Liquidus), °C 660
1470
Melting Onset (Solidus), °C 650
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 230
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.8
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.7
Embodied Energy, MJ/kg 160
23
Embodied Water, L/kg 1200
58

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
83
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
140
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.0 to 19
18
Strength to Weight: Bending, points 14 to 27
18
Thermal Diffusivity, mm2/s 96
11
Thermal Shock Resistance, points 3.0 to 8.2
14

Alloy Composition


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Aluminum (Al), % 99.5 to 100
0
Boron (B), % 0 to 0.050
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.010
2.0 to 2.5
Copper (Cu), % 0 to 0.050
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
95.2 to 96.8
Manganese (Mn), % 0 to 0.010
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.020
0
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.1
0