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R58150 Titanium vs. 7475 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 7475 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 7475 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
70
Elongation at Break, % 13
10 to 12
Fatigue Strength, MPa 330
190 to 210
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
320 to 350
Tensile Strength: Ultimate (UTS), MPa 770
530 to 590
Tensile Strength: Yield (Proof), MPa 550
440 to 520

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
53 to 68
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
1390 to 1920
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 32
46
Strength to Weight: Axial, points 40
49 to 55
Strength to Weight: Bending, points 35
48 to 52
Thermal Shock Resistance, points 48
23 to 26

Alloy Composition

Aluminum (Al), % 0
88.6 to 91.6
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0.18 to 0.25
Copper (Cu), % 0
1.2 to 1.9
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.12
Magnesium (Mg), % 0
1.9 to 2.6
Manganese (Mn), % 0
0 to 0.060
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 0.1
Titanium (Ti), % 83.5 to 86
0 to 0.060
Zinc (Zn), % 0
5.1 to 6.2
Residuals, % 0
0 to 0.15