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ASTM A369 Grade FP92 vs. 6016 Aluminum

ASTM A369 grade FP92 belongs to the iron alloys classification, while 6016 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 A369 grade FP92 and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
55 to 80
Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 19
11 to 27
Fatigue Strength, MPa 330
68 to 89
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 440
130 to 170
Tensile Strength: Ultimate (UTS), MPa 710
200 to 280
Tensile Strength: Yield (Proof), MPa 490
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 260
410
Maximum Temperature: Mechanical, °C 590
160
Melting Completion (Liquidus), °C 1490
660
Melting Onset (Solidus), °C 1450
610
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 26
190 to 210
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 10
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 2.8
8.2
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 89
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 620
82 to 340
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 25
21 to 29
Strength to Weight: Bending, points 22
29 to 35
Thermal Diffusivity, mm2/s 6.9
77 to 86
Thermal Shock Resistance, points 19
9.1 to 12

Alloy Composition


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Aluminum (Al), % 0 to 0.020
96.4 to 98.8
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 85.8 to 89.1
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0.3 to 0.6
0 to 0.2
Molybdenum (Mo), % 0.3 to 0.6
0
Nickel (Ni), % 0 to 0.4
0
Niobium (Nb), % 0.040 to 0.090
0
Nitrogen (N), % 0.030 to 0.070
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
1.0 to 1.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.15
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15