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R30035 Cobalt vs. 1050 Aluminum

R30035 cobalt belongs to the cobalt alloys classification, while 1050 aluminum belongs to the aluminum alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, 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 1050 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220 to 230
68
Elongation at Break, % 9.0 to 46
4.6 to 37
Fatigue Strength, MPa 170 to 740
31 to 57
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 84 to 89
26
Tensile Strength: Ultimate (UTS), MPa 900 to 1900
76 to 140
Tensile Strength: Yield (Proof), MPa 300 to 1650
25 to 120

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Melting Completion (Liquidus), °C 1440
640
Melting Onset (Solidus), °C 1320
650
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 11
230
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
61
Electrical Conductivity: Equal Weight (Specific), % IACS 1.8
200

Otherwise Unclassified Properties

Base Metal Price, % relative 100
9.5
Density, g/cm3 8.7
2.7
Embodied Carbon, kg CO2/kg material 10
8.3
Embodied Energy, MJ/kg 140
160
Embodied Water, L/kg 410
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160 to 320
5.4 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 5920
4.6 to 110
Stiffness to Weight: Axial, points 14 to 15
14
Stiffness to Weight: Bending, points 23 to 24
50
Strength to Weight: Axial, points 29 to 61
7.8 to 14
Strength to Weight: Bending, points 24 to 39
15 to 22
Thermal Diffusivity, mm2/s 3.0
94
Thermal Shock Resistance, points 23 to 46
3.4 to 6.2

Alloy Composition

Aluminum (Al), % 0
99.5 to 100
Boron (B), % 0 to 0.015
0
Carbon (C), % 0 to 0.025
0
Chromium (Cr), % 19 to 21
0
Cobalt (Co), % 29.1 to 39
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 0 to 1.0
0 to 0.4
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 0.15
0 to 0.050
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 0.25
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 1.0
0 to 0.030
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050

Comparable Variants