MakeItFrom.com
Menu (ESC)

R58150 Titanium vs. 850.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 850.0 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is R58150 titanium and the bottom bar is 850.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
69
Elongation at Break, % 13
7.9
Fatigue Strength, MPa 330
59
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
26
Shear Strength, MPa 470
100
Tensile Strength: Ultimate (UTS), MPa 770
140
Tensile Strength: Yield (Proof), MPa 550
76

Thermal Properties

Latent Heat of Fusion, J/g 410
380
Maximum Temperature: Mechanical, °C 320
190
Melting Completion (Liquidus), °C 1760
650
Melting Onset (Solidus), °C 1700
370
Specific Heat Capacity, J/kg-K 500
850
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
14
Density, g/cm3 5.4
3.1
Embodied Carbon, kg CO2/kg material 31
8.5
Embodied Energy, MJ/kg 480
160
Embodied Water, L/kg 150
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
9.1
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
42
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 32
44
Strength to Weight: Axial, points 40
12
Strength to Weight: Bending, points 35
19
Thermal Shock Resistance, points 48
6.1

Alloy Composition

Aluminum (Al), % 0
88.3 to 93.1
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0.7 to 1.3
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.7
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0
0 to 0.1
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0.7 to 1.3
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.7
Tin (Sn), % 0
5.5 to 7.0
Titanium (Ti), % 83.5 to 86
0 to 0.2
Residuals, % 0
0 to 0.3