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Sintered 6061 Aluminum vs. R58150 Titanium

Sintered 6061 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 sintered 6061 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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