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C36200 Brass vs. Titanium 6-7

C36200 brass belongs to the copper alloys classification, while titanium 6-7 belongs to the titanium alloys. There are 25 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 C36200 brass and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
120
Elongation at Break, % 20 to 53
11
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 39
45
Shear Strength, MPa 210 to 240
610
Tensile Strength: Ultimate (UTS), MPa 340 to 420
1020
Tensile Strength: Yield (Proof), MPa 130 to 360
900

Thermal Properties

Latent Heat of Fusion, J/g 170
410
Maximum Temperature: Mechanical, °C 120
300
Melting Completion (Liquidus), °C 900
1700
Melting Onset (Solidus), °C 890
1650
Specific Heat Capacity, J/kg-K 380
520
Thermal Expansion, µm/m-K 21
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 23
75
Density, g/cm3 8.2
5.1
Embodied Carbon, kg CO2/kg material 2.6
34
Embodied Energy, MJ/kg 45
540
Embodied Water, L/kg 320
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 140
110
Resilience: Unit (Modulus of Resilience), kJ/m3 89 to 630
3460
Stiffness to Weight: Axial, points 6.9
13
Stiffness to Weight: Bending, points 19
32
Strength to Weight: Axial, points 11 to 14
56
Strength to Weight: Bending, points 13 to 15
44
Thermal Shock Resistance, points 11 to 14
66

Alloy Composition

Aluminum (Al), % 0
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 60 to 63
0
Hydrogen (H), % 0
0 to 0.0090
Iron (Fe), % 0 to 0.15
0 to 0.25
Lead (Pb), % 3.5 to 4.5
0
Molybdenum (Mo), % 0
6.5 to 7.5
Niobium (Nb), % 0
6.5 to 7.5
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Tantalum (Ta), % 0
0 to 0.5
Titanium (Ti), % 0
84.9 to 88
Zinc (Zn), % 32.4 to 36.5
0