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1350 Aluminum vs. ASTM A229 Spring Steel

1350 aluminum belongs to the aluminum alloys classification, while ASTM A229 spring steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 A229 spring steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 20 to 45
490 to 550
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.4 to 30
14
Fatigue Strength, MPa 24 to 50
710 to 790
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 44 to 110
1020 to 1140
Tensile Strength: Ultimate (UTS), MPa 68 to 190
1690 to 1890
Tensile Strength: Yield (Proof), MPa 25 to 170
1100 to 1230

Thermal Properties

Latent Heat of Fusion, J/g 400
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 660
1450
Melting Onset (Solidus), °C 650
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 230
50
Thermal Expansion, µm/m-K 24
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.8
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.4
Embodied Energy, MJ/kg 160
19
Embodied Water, L/kg 1200
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
200 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
3260 to 4080
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 7.0 to 19
60 to 67
Strength to Weight: Bending, points 14 to 27
40 to 43
Thermal Diffusivity, mm2/s 96
14
Thermal Shock Resistance, points 3.0 to 8.2
54 to 60

Alloy Composition

Aluminum (Al), % 99.5 to 100
0
Boron (B), % 0 to 0.050
0
Carbon (C), % 0
0.55 to 0.85
Chromium (Cr), % 0 to 0.010
0
Copper (Cu), % 0 to 0.050
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
97.5 to 99
Manganese (Mn), % 0 to 0.010
0.3 to 1.2
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0.15 to 0.35
Sulfur (S), % 0
0 to 0.050
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

Comparable Variants