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R58150 Titanium vs. 7178 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 7178 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 7178 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
71
Elongation at Break, % 13
4.5 to 12
Fatigue Strength, MPa 330
120 to 210
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
140 to 380
Tensile Strength: Ultimate (UTS), MPa 770
240 to 640
Tensile Strength: Yield (Proof), MPa 550
120 to 560

Thermal Properties

Latent Heat of Fusion, J/g 410
370
Maximum Temperature: Mechanical, °C 320
180
Melting Completion (Liquidus), °C 1760
630
Melting Onset (Solidus), °C 1700
480
Specific Heat Capacity, J/kg-K 500
860
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
10
Density, g/cm3 5.4
3.1
Embodied Carbon, kg CO2/kg material 31
8.2
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
24 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
110 to 2220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
45
Strength to Weight: Axial, points 40
21 to 58
Strength to Weight: Bending, points 35
28 to 54
Thermal Shock Resistance, points 48
10 to 28

Alloy Composition


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Aluminum (Al), % 0
85.4 to 89.5
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0.18 to 0.28
Copper (Cu), % 0
1.6 to 2.4
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.5
Magnesium (Mg), % 0
2.4 to 3.1
Manganese (Mn), % 0
0 to 0.3
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
6.3 to 7.3
Residuals, % 0
0 to 0.15