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ASTM A372 Grade M Steel vs. 332.0 Aluminum

ASTM A372 grade M steel belongs to the iron alloys classification, while 332.0 aluminum belongs to the aluminum 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 ASTM A372 grade M steel and the bottom bar is 332.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 240 to 280
110
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 18 to 21
1.0
Fatigue Strength, MPa 450 to 520
90
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
27
Shear Strength, MPa 510 to 570
190
Tensile Strength: Ultimate (UTS), MPa 810 to 910
250
Tensile Strength: Yield (Proof), MPa 660 to 770
190

Thermal Properties

Latent Heat of Fusion, J/g 250
530
Maximum Temperature: Mechanical, °C 450
170
Melting Completion (Liquidus), °C 1460
580
Melting Onset (Solidus), °C 1420
530
Specific Heat Capacity, J/kg-K 470
880
Thermal Conductivity, W/m-K 46
100
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.0
26
Electrical Conductivity: Equal Weight (Specific), % IACS 9.1
84

Otherwise Unclassified Properties

Base Metal Price, % relative 5.0
10
Density, g/cm3 7.9
2.8
Embodied Carbon, kg CO2/kg material 2.0
7.8
Embodied Energy, MJ/kg 27
140
Embodied Water, L/kg 61
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 1140 to 1580
250
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 29 to 32
24
Strength to Weight: Bending, points 24 to 27
31
Thermal Diffusivity, mm2/s 12
42
Thermal Shock Resistance, points 24 to 27
12

Alloy Composition

Aluminum (Al), % 0
80.1 to 89
Carbon (C), % 0 to 0.23
0
Chromium (Cr), % 1.5 to 2.0
0
Copper (Cu), % 0
2.0 to 4.0
Iron (Fe), % 92.5 to 95.1
0 to 1.2
Magnesium (Mg), % 0
0.5 to 1.5
Manganese (Mn), % 0.2 to 0.4
0 to 0.5
Molybdenum (Mo), % 0.4 to 0.6
0
Nickel (Ni), % 2.8 to 3.9
0 to 0.5
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.3
8.5 to 10.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.25
Vanadium (V), % 0 to 0.080
0
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5