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R30035 Cobalt vs. 7050 Aluminum

R30035 cobalt belongs to the cobalt alloys classification, while 7050 aluminum belongs to the aluminum alloys. There are 28 material properties with values for both materials. Properties with values for just one material (3, 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 R30035 cobalt and the bottom bar is 7050 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220 to 230
70
Elongation at Break, % 9.0 to 46
2.2 to 12
Fatigue Strength, MPa 170 to 740
130 to 210
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 84 to 89
26
Tensile Strength: Ultimate (UTS), MPa 900 to 1900
490 to 570
Tensile Strength: Yield (Proof), MPa 300 to 1650
390 to 500

Thermal Properties

Latent Heat of Fusion, J/g 320
370
Melting Completion (Liquidus), °C 1440
630
Melting Onset (Solidus), °C 1320
490
Specific Heat Capacity, J/kg-K 440
860
Thermal Conductivity, W/m-K 11
140
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
35
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
100

Otherwise Unclassified Properties

Base Metal Price, % relative 100
10
Density, g/cm3 8.7
3.1
Embodied Carbon, kg CO2/kg material 10
8.2
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 410
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160 to 320
10 to 55
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 5920
1110 to 1760
Stiffness to Weight: Axial, points 14 to 15
13
Stiffness to Weight: Bending, points 23 to 24
45
Strength to Weight: Axial, points 29 to 61
45 to 51
Strength to Weight: Bending, points 24 to 39
45 to 50
Thermal Diffusivity, mm2/s 3.0
54
Thermal Shock Resistance, points 23 to 46
21 to 25

Alloy Composition


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Aluminum (Al), % 0
87.3 to 92.1
Boron (B), % 0 to 0.015
0
Carbon (C), % 0 to 0.025
0
Chromium (Cr), % 19 to 21
0 to 0.040
Cobalt (Co), % 29.1 to 39
0
Copper (Cu), % 0
2.0 to 2.6
Iron (Fe), % 0 to 1.0
0 to 0.15
Magnesium (Mg), % 0
1.9 to 2.6
Manganese (Mn), % 0 to 0.15
0 to 0.1
Molybdenum (Mo), % 9.0 to 10.5
0
Nickel (Ni), % 33 to 37
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.15
0 to 0.12
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 1.0
0 to 0.060
Zinc (Zn), % 0
5.7 to 6.7
Zirconium (Zr), % 0
0.080 to 0.15
Residuals, % 0
0 to 0.15