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R58150 Titanium vs. Sintered 6061 Aluminum

R58150 titanium belongs to the titanium alloys classification, while sintered 6061 aluminum belongs to the aluminum alloys. There are 25 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 sintered 6061 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
68
Elongation at Break, % 13
0.5 to 6.0
Fatigue Strength, MPa 330
32 to 62
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
25
Tensile Strength: Ultimate (UTS), MPa 770
83 to 210
Tensile Strength: Yield (Proof), MPa 550
62 to 190

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
640
Melting Onset (Solidus), °C 1700
610
Specific Heat Capacity, J/kg-K 500
900
Thermal Expansion, µm/m-K 8.4
23

Otherwise Unclassified Properties

Base Metal Price, % relative 48
9.5
Density, g/cm3 5.4
2.7
Embodied Carbon, kg CO2/kg material 31
8.3
Embodied Energy, MJ/kg 480
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
0.68 to 7.0
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
28 to 280
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 40
8.6 to 21
Strength to Weight: Bending, points 35
16 to 29
Thermal Shock Resistance, points 48
3.8 to 9.4

Alloy Composition

Aluminum (Al), % 0
96 to 99.4
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
0 to 0.5
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0
Magnesium (Mg), % 0
0.4 to 1.2
Molybdenum (Mo), % 14 to 16
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0.2 to 0.8
Titanium (Ti), % 83.5 to 86
0
Residuals, % 0
0 to 1.5