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R58150 Titanium vs. 336.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 336.0 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 336.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
75
Elongation at Break, % 13
0.5
Fatigue Strength, MPa 330
80 to 93
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
28
Shear Strength, MPa 470
190 to 250
Tensile Strength: Ultimate (UTS), MPa 770
250 to 320
Tensile Strength: Yield (Proof), MPa 550
190 to 300

Thermal Properties

Latent Heat of Fusion, J/g 410
570
Maximum Temperature: Mechanical, °C 320
210
Melting Completion (Liquidus), °C 1760
570
Melting Onset (Solidus), °C 1700
540
Specific Heat Capacity, J/kg-K 500
890
Thermal Expansion, µm/m-K 8.4
19

Otherwise Unclassified Properties

Base Metal Price, % relative 48
11
Density, g/cm3 5.4
2.8
Embodied Carbon, kg CO2/kg material 31
7.9
Embodied Energy, MJ/kg 480
140
Embodied Water, L/kg 150
1010

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
1.1 to 1.6
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
250 to 580
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 40
25 to 32
Strength to Weight: Bending, points 35
32 to 38
Thermal Shock Resistance, points 48
12 to 16

Alloy Composition

Aluminum (Al), % 0
79.1 to 85.8
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0.5 to 1.5
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.2
Magnesium (Mg), % 0
0.7 to 1.3
Manganese (Mn), % 0
0 to 0.35
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
2.0 to 3.0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
11 to 13
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
0 to 0.35