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850.0 Aluminum vs. R58150 Titanium

850.0 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium alloys. There are 26 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is 850.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
140
Elongation at Break, % 7.9
13
Fatigue Strength, MPa 59
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 100
470
Tensile Strength: Ultimate (UTS), MPa 140
770
Tensile Strength: Yield (Proof), MPa 76
550

Thermal Properties

Latent Heat of Fusion, J/g 380
410
Maximum Temperature: Mechanical, °C 190
320
Melting Completion (Liquidus), °C 650
1760
Melting Onset (Solidus), °C 370
1700
Specific Heat Capacity, J/kg-K 850
500
Thermal Expansion, µm/m-K 23
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 14
48
Density, g/cm3 3.1
5.4
Embodied Carbon, kg CO2/kg material 8.5
31
Embodied Energy, MJ/kg 160
480
Embodied Water, L/kg 1160
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.1
94
Resilience: Unit (Modulus of Resilience), kJ/m3 42
1110
Stiffness to Weight: Axial, points 12
14
Stiffness to Weight: Bending, points 44
32
Strength to Weight: Axial, points 12
40
Strength to Weight: Bending, points 19
35
Thermal Shock Resistance, points 6.1
48

Alloy Composition


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Aluminum (Al), % 88.3 to 93.1
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0.7 to 1.3
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.7
0 to 0.1
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.1
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0.7 to 1.3
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.7
0
Tin (Sn), % 5.5 to 7.0
0
Titanium (Ti), % 0 to 0.2
83.5 to 86
Residuals, % 0 to 0.3
0