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Titanium 6-7 vs. C85200 Brass

Titanium 6-7 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 titanium 6-7 and the bottom bar is C85200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
110
Elongation at Break, % 11
28
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 45
40
Tensile Strength: Ultimate (UTS), MPa 1020
270
Tensile Strength: Yield (Proof), MPa 900
95

Thermal Properties

Latent Heat of Fusion, J/g 410
180
Maximum Temperature: Mechanical, °C 300
140
Melting Completion (Liquidus), °C 1700
940
Melting Onset (Solidus), °C 1650
930
Specific Heat Capacity, J/kg-K 520
380
Thermal Expansion, µm/m-K 9.3
20

Otherwise Unclassified Properties

Base Metal Price, % relative 75
26
Density, g/cm3 5.1
8.4
Embodied Carbon, kg CO2/kg material 34
2.8
Embodied Energy, MJ/kg 540
46
Embodied Water, L/kg 190
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
59
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
42
Stiffness to Weight: Axial, points 13
7.0
Stiffness to Weight: Bending, points 32
19
Strength to Weight: Axial, points 56
8.9
Strength to Weight: Bending, points 44
11
Thermal Shock Resistance, points 66
9.3

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
0 to 0.0050
Antimony (Sb), % 0
0 to 0.2
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
70 to 74
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.6
Lead (Pb), % 0
1.5 to 3.8
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 1.0
Niobium (Nb), % 6.5 to 7.5
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
Tantalum (Ta), % 0 to 0.5
0
Tin (Sn), % 0
0.7 to 2.0
Titanium (Ti), % 84.9 to 88
0
Zinc (Zn), % 0
20 to 27
Residuals, % 0
0 to 0.9