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6262A Aluminum vs. ASTM A369 Grade FP92

6262A aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP92 belongs to the iron alloys. There are 30 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 6262A aluminum and the bottom bar is ASTM A369 grade FP92.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 4.5 to 11
19
Fatigue Strength, MPa 94 to 110
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 190 to 240
440
Tensile Strength: Ultimate (UTS), MPa 310 to 410
710
Tensile Strength: Yield (Proof), MPa 270 to 370
490

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 160
590
Melting Completion (Liquidus), °C 640
1490
Melting Onset (Solidus), °C 580
1450
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 170
26
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 45
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
10

Otherwise Unclassified Properties

Base Metal Price, % relative 11
11
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 8.4
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1190
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 34
120
Resilience: Unit (Modulus of Resilience), kJ/m3 540 to 1000
620
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 31 to 41
25
Strength to Weight: Bending, points 36 to 44
22
Thermal Diffusivity, mm2/s 67
6.9
Thermal Shock Resistance, points 14 to 18
19

Alloy Composition

Aluminum (Al), % 94.2 to 97.8
0 to 0.020
Bismuth (Bi), % 0.4 to 0.9
0
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0.040 to 0.14
8.5 to 9.5
Copper (Cu), % 0.15 to 0.4
0
Iron (Fe), % 0 to 0.7
85.8 to 89.1
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0 to 0.15
0.3 to 0.6
Molybdenum (Mo), % 0
0.3 to 0.6
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.040 to 0.090
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.4 to 0.8
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0.4 to 1.0
0
Titanium (Ti), % 0 to 0.1
0 to 0.010
Tungsten (W), % 0
1.5 to 2.0
Vanadium (V), % 0
0.15 to 0.25
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.15
0