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ASTM A387 Grade 21 Steel vs. 7076 Aluminum

ASTM A387 grade 21 steel belongs to the iron alloys classification, while 7076 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 A387 grade 21 steel and the bottom bar is 7076 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150 to 180
160
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 21
6.2
Fatigue Strength, MPa 160 to 250
170
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 74
27
Shear Strength, MPa 310 to 370
310
Tensile Strength: Ultimate (UTS), MPa 500 to 590
530
Tensile Strength: Yield (Proof), MPa 230 to 350
460

Thermal Properties

Latent Heat of Fusion, J/g 260
380
Maximum Temperature: Mechanical, °C 480
170
Melting Completion (Liquidus), °C 1470
630
Melting Onset (Solidus), °C 1430
460
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 41
140
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
35
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
100

Otherwise Unclassified Properties

Base Metal Price, % relative 4.1
9.5
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 1.8
8.0
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 62
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 84 to 110
31
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 320
1510
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 18 to 21
49
Strength to Weight: Bending, points 18 to 20
48
Thermal Diffusivity, mm2/s 11
54
Thermal Shock Resistance, points 14 to 17
23

Alloy Composition

Aluminum (Al), % 0
86.9 to 91.2
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 2.8 to 3.3
0
Copper (Cu), % 0
0.3 to 1.0
Iron (Fe), % 94.4 to 96
0 to 0.6
Magnesium (Mg), % 0
1.2 to 2.0
Manganese (Mn), % 0.3 to 0.6
0.3 to 0.8
Molybdenum (Mo), % 0.9 to 1.1
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.15