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R58150 Titanium vs. C85200 Brass

R58150 titanium belongs to the titanium alloys classification, while C85200 brass belongs to the copper alloys. There are 24 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 C85200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
110
Elongation at Break, % 13
28
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 52
40
Tensile Strength: Ultimate (UTS), MPa 770
270
Tensile Strength: Yield (Proof), MPa 550
95

Thermal Properties

Latent Heat of Fusion, J/g 410
180
Maximum Temperature: Mechanical, °C 320
140
Melting Completion (Liquidus), °C 1760
940
Melting Onset (Solidus), °C 1700
930
Specific Heat Capacity, J/kg-K 500
380
Thermal Expansion, µm/m-K 8.4
20

Otherwise Unclassified Properties

Base Metal Price, % relative 48
26
Density, g/cm3 5.4
8.4
Embodied Carbon, kg CO2/kg material 31
2.8
Embodied Energy, MJ/kg 480
46
Embodied Water, L/kg 150
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
59
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
42
Stiffness to Weight: Axial, points 14
7.0
Stiffness to Weight: Bending, points 32
19
Strength to Weight: Axial, points 40
8.9
Strength to Weight: Bending, points 35
11
Thermal Shock Resistance, points 48
9.3

Alloy Composition

Aluminum (Al), % 0
0 to 0.0050
Antimony (Sb), % 0
0 to 0.2
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
70 to 74
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 0.6
Lead (Pb), % 0
1.5 to 3.8
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 1.0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0
0 to 0.050
Sulfur (S), % 0
0 to 0.050
Tin (Sn), % 0
0.7 to 2.0
Titanium (Ti), % 83.5 to 86
0
Zinc (Zn), % 0
20 to 27
Residuals, % 0
0 to 0.9