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R58150 Titanium vs. 705.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 705.0 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 705.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
8.4 to 10
Fatigue Strength, MPa 330
63 to 98
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Tensile Strength: Ultimate (UTS), MPa 770
240 to 260
Tensile Strength: Yield (Proof), MPa 550
130

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 320
180
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
610
Specific Heat Capacity, J/kg-K 500
890
Thermal Expansion, µm/m-K 8.4
24

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.8
Embodied Carbon, kg CO2/kg material 31
8.4
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
18 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
120 to 130
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
49
Strength to Weight: Axial, points 40
24 to 26
Strength to Weight: Bending, points 35
31 to 32
Thermal Shock Resistance, points 48
11

Alloy Composition

Aluminum (Al), % 0
92.3 to 98.6
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.4
Copper (Cu), % 0
0 to 0.2
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.8
Magnesium (Mg), % 0
1.4 to 1.8
Manganese (Mn), % 0
0 to 0.6
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.2
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
0 to 3.3
Residuals, % 0
0 to 0.15