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Nickel 890 vs. C83300 Brass

Nickel 890 belongs to the nickel alloys classification, while C83300 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 C83300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
110
Elongation at Break, % 39
35
Poisson's Ratio 0.28
0.34
Shear Modulus, GPa 78
42
Tensile Strength: Ultimate (UTS), MPa 590
220
Tensile Strength: Yield (Proof), MPa 230
69

Thermal Properties

Latent Heat of Fusion, J/g 330
200
Maximum Temperature: Mechanical, °C 1000
180
Melting Completion (Liquidus), °C 1390
1060
Melting Onset (Solidus), °C 1340
1030
Specific Heat Capacity, J/kg-K 480
380
Thermal Expansion, µm/m-K 14
18

Otherwise Unclassified Properties

Base Metal Price, % relative 47
30
Density, g/cm3 8.1
8.8
Embodied Carbon, kg CO2/kg material 8.2
2.7
Embodied Energy, MJ/kg 120
44
Embodied Water, L/kg 250
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
60
Resilience: Unit (Modulus of Resilience), kJ/m3 140
21
Stiffness to Weight: Axial, points 14
7.0
Stiffness to Weight: Bending, points 24
18
Strength to Weight: Axial, points 20
6.9
Strength to Weight: Bending, points 19
9.2
Thermal Shock Resistance, points 15
7.9

Alloy Composition

Aluminum (Al), % 0.050 to 0.6
0
Carbon (C), % 0.060 to 0.14
0
Chromium (Cr), % 23.5 to 28.5
0
Copper (Cu), % 0 to 0.75
92 to 94
Iron (Fe), % 17.3 to 33.9
0
Lead (Pb), % 0
1.0 to 2.0
Manganese (Mn), % 0 to 1.5
0
Molybdenum (Mo), % 1.0 to 2.0
0
Nickel (Ni), % 40 to 45
0
Niobium (Nb), % 0.2 to 1.0
0
Silicon (Si), % 1.0 to 2.0
0
Sulfur (S), % 0 to 0.015
0
Tantalum (Ta), % 0.1 to 0.6
0
Tin (Sn), % 0
1.0 to 2.0
Titanium (Ti), % 0.15 to 0.6
0
Zinc (Zn), % 0
2.0 to 6.0
Residuals, % 0
0 to 0.7