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R58150 Titanium vs. 7076 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 7076 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 7076 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
6.2
Fatigue Strength, MPa 330
170
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
310
Tensile Strength: Ultimate (UTS), MPa 770
530
Tensile Strength: Yield (Proof), MPa 550
460

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
630
Melting Onset (Solidus), °C 1700
460
Specific Heat Capacity, J/kg-K 500
860
Thermal Expansion, µm/m-K 8.4
24

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
3.0
Embodied Carbon, kg CO2/kg material 31
8.0
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
31
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
1510
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
45
Strength to Weight: Axial, points 40
49
Strength to Weight: Bending, points 35
48
Thermal Shock Resistance, points 48
23

Alloy Composition

Aluminum (Al), % 0
86.9 to 91.2
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0.3 to 1.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.6
Magnesium (Mg), % 0
1.2 to 2.0
Manganese (Mn), % 0
0.3 to 0.8
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 0.4
Titanium (Ti), % 83.5 to 86
0 to 0.2
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.15