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Nickel 890 vs. CC767S Brass

Nickel 890 belongs to the nickel alloys classification, while CC767S 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 nickel 890 and the bottom bar is CC767S brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
110
Elongation at Break, % 39
34
Poisson's Ratio 0.28
0.31
Shear Modulus, GPa 78
40
Tensile Strength: Ultimate (UTS), MPa 590
430
Tensile Strength: Yield (Proof), MPa 230
150

Thermal Properties

Latent Heat of Fusion, J/g 330
180
Maximum Temperature: Mechanical, °C 1000
120
Melting Completion (Liquidus), °C 1390
840
Melting Onset (Solidus), °C 1340
790
Specific Heat Capacity, J/kg-K 480
390
Thermal Expansion, µm/m-K 14
21

Otherwise Unclassified Properties

Base Metal Price, % relative 47
23
Density, g/cm3 8.1
8.0
Embodied Carbon, kg CO2/kg material 8.2
2.7
Embodied Energy, MJ/kg 120
47
Embodied Water, L/kg 250
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
110
Resilience: Unit (Modulus of Resilience), kJ/m3 140
100
Stiffness to Weight: Axial, points 14
7.3
Stiffness to Weight: Bending, points 24
20
Strength to Weight: Axial, points 20
15
Strength to Weight: Bending, points 19
16
Thermal Shock Resistance, points 15
14

Alloy Composition

Aluminum (Al), % 0.050 to 0.6
0.1 to 0.8
Carbon (C), % 0.060 to 0.14
0
Chromium (Cr), % 23.5 to 28.5
0
Copper (Cu), % 0 to 0.75
58 to 64
Iron (Fe), % 17.3 to 33.9
0 to 0.5
Lead (Pb), % 0
0 to 0.1
Manganese (Mn), % 0 to 1.5
0 to 0.5
Molybdenum (Mo), % 1.0 to 2.0
0
Nickel (Ni), % 40 to 45
0 to 1.0
Niobium (Nb), % 0.2 to 1.0
0
Silicon (Si), % 1.0 to 2.0
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Tantalum (Ta), % 0.1 to 0.6
0
Tin (Sn), % 0
0 to 0.1
Titanium (Ti), % 0.15 to 0.6
0
Zinc (Zn), % 0
32.8 to 41.9