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7175 Aluminum vs. R58150 Titanium

7175 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 (5, in this case) are not shown.

For each property being compared, the top bar is 7175 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
140
Elongation at Break, % 3.8 to 5.9
13
Fatigue Strength, MPa 150 to 180
330
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 26
52
Shear Strength, MPa 290 to 330
470
Tensile Strength: Ultimate (UTS), MPa 520 to 570
770
Tensile Strength: Yield (Proof), MPa 430 to 490
550

Thermal Properties

Latent Heat of Fusion, J/g 380
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 640
1760
Melting Onset (Solidus), °C 480
1700
Specific Heat Capacity, J/kg-K 870
500
Thermal Expansion, µm/m-K 23
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
48
Density, g/cm3 3.0
5.4
Embodied Carbon, kg CO2/kg material 8.2
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1130
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 18 to 29
94
Resilience: Unit (Modulus of Resilience), kJ/m3 1310 to 1730
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
32
Strength to Weight: Axial, points 48 to 52
40
Strength to Weight: Bending, points 48 to 51
35
Thermal Shock Resistance, points 23 to 25
48

Alloy Composition


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Aluminum (Al), % 88 to 91.4
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.18 to 0.28
0
Copper (Cu), % 1.2 to 2.0
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.2
0 to 0.1
Magnesium (Mg), % 2.1 to 2.9
0
Manganese (Mn), % 0 to 0.1
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.1
83.5 to 86
Zinc (Zn), % 5.1 to 6.1
0
Residuals, % 0 to 0.15
0