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R58150 Titanium vs. 7021 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 7021 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 7021 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
9.4
Fatigue Strength, MPa 330
150
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
270
Tensile Strength: Ultimate (UTS), MPa 770
460
Tensile Strength: Yield (Proof), MPa 550
390

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 320
200
Melting Completion (Liquidus), °C 1760
630
Melting Onset (Solidus), °C 1700
510
Specific Heat Capacity, J/kg-K 500
870
Thermal Expansion, µm/m-K 8.4
24

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.9
Embodied Carbon, kg CO2/kg material 31
8.3
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
41
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
1110
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
47
Strength to Weight: Axial, points 40
44
Strength to Weight: Bending, points 35
45
Thermal Shock Resistance, points 48
20

Alloy Composition

Aluminum (Al), % 0
90.7 to 93.7
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.050
Copper (Cu), % 0
0 to 0.25
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.4
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 0
0 to 0.1
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 0.25
Titanium (Ti), % 83.5 to 86
0 to 0.1
Zinc (Zn), % 0
5.0 to 6.0
Zirconium (Zr), % 0
0.080 to 0.18
Residuals, % 0
0 to 0.15