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Material Comparison Engine

Compare verified materials with source-specific conditions, units, and property limits.

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1. Identity, Classification & Standards
ParameterC63200 Nickel-Aluminum Bronze (Naval Alloy)C14500 Tellurium Copper
Material FamilyCopper AlloysCopper Alloys
SubfamilyAluminum BronzeFree-Machining Copper
UNS DesignationC63200C14500
COMMERCIAL DesignationNickel-Aluminum Bronze (Naval Alloy)Tellurium Copper
CDA DesignationAlloy 632Alloy 145
SPECIFICATION DesignationASTM B124/B124MASTM B224
2. Chemical Composition Limits (wt %)Source-specific limits and typical values
ElementC63200 Nickel-Aluminum Bronze (Naval Alloy)C14500 Tellurium Copper
Cu (Copper)Bal.≥ 99.9%
Pb (Lead)≤ 0.02%—
Fe (Iron)3.5 – 4.3%—
Ni (Nickel)4 – 4.8%—
Al (Aluminum)8.7 – 9.5%—
Mn (Manganese)1.2 – 2%—
Si (Silicon)≤ 0.1%—
P (Phosphorus)—0.004 – 0.012%
Te (Tellurium)—0.4 – 0.7%
3. Physical Properties
PropertyC63200 Nickel-Aluminum Bronze (Naval Alloy)C14500 Tellurium Copper
Density · TYPICAL · 20 °CUnit: g/cm³7.64 g/cm³8.941 g/cm³
4. Contextual Mechanical PropertiesUnit: SI
Mechanical ParameterC63200 Nickel-Aluminum Bronze (Naval Alloy)Light Anneal (O50)C14500 Tellurium Copper1/2 Hard (H02)
Modulus of Elasticity (Tension) · TYPICALUnit: GPa117.2 GPa117.2 GPa
Modulus of Rigidity · TYPICALUnit: MPa44126.4 MPa44126.4 MPa
Machinability Rating · TYPICALUnit: %30 %85 %
Forgeability Rating · TYPICALUnit: —70 —65 —
Tensile Strength · Forgings · 5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa689.5 MPa— MPa
Tensile Strength · Plate · 0.5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa655 MPa— MPa
Tensile Strength · Plate · 0.25 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa689.5 MPa— MPa
Tensile Strength · Plate · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa620.5 MPa— MPa
Tensile Strength · Rod · 2 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa710.2 MPa— MPa
Tensile Strength · Rod · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa723.9 MPa— MPa
Tensile Strength · Rod · 3 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa703.3 MPa— MPa
Tensile Strength · Rod · 0.25 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa262 MPa
Tensile Strength · Rod · .0625 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa262 MPa
Tensile Strength · Rod · 1 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa289.6 MPa
Tensile Strength · Rod · 1 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa289.6 MPa
Tensile Strength · Rod · .25 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa262 MPa
Tensile Strength · Rod · 2 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa289.6 MPa
Tensile Strength · Rod · 2 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa289.6 MPa
Tensile Strength · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa296.5 MPa
Tensile Strength · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa296.5 MPa
Tensile Strength · Rod · 0.24 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa296.5 MPa
Tensile Strength · Wire · 0.08 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa351.6 MPa
Yield Strength (0.5% Ext) · Forgings · 5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa310.3 MPa— MPa
Yield Strength (0.5% Ext) · Plate · 0.5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa324.1 MPa— MPa
Yield Strength (0.5% Ext) · Plate · 0.25 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa344.7 MPa— MPa
Yield Strength (0.5% Ext) · Plate · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa310.3 MPa— MPa
Yield Strength (0.5% Ext) · Rod · 2 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa358.5 MPa— MPa
Yield Strength (0.5% Ext) · Rod · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa365.4 MPa— MPa
Yield Strength (0.5% Ext) · Rod · 3 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa351.6 MPa— MPa
Yield Strength (0.5% Ext) · Rod · 1 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa275.8 MPa
Yield Strength (0.5% Ext) · Rod · 1 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa275.8 MPa
Yield Strength (0.5% Ext) · Rod · 2 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa268.9 MPa
Yield Strength (0.5% Ext) · Rod · 2 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa268.9 MPa
Yield Strength (0.5% Ext) · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa275.8 MPa
Yield Strength (0.5% Ext) · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa275.8 MPa
Yield Strength (0.5% Ext) · Rod · 0.24 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa275.8 MPa
Yield Strength (0.5% Ext) · Wire · 0.08 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: MPa— MPa282.7 MPa
Elongation · Forgings · 5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %22 %— %
Elongation · Plate · 0.5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %22 %— %
Elongation · Plate · 0.25 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %20 %— %
Elongation · Plate · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %25 %— %
Elongation · Rod · 2 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %24 %— %
Elongation · Rod · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %22 %— %
Elongation · Rod · 3 · Light Anneal (O50) · TYPICAL · 20 °CUnit: %24 %— %
Elongation · Rod · 0.25 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %18 %
Elongation · Rod · .0625 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %8 %
Elongation · Rod · 1 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %25 %
Elongation · Rod · 1 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %25 %
Elongation · Rod · .25 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %12 %
Elongation · Rod · 2 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %35 %
Elongation · Rod · 2 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %35 %
Elongation · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %20 %
Elongation · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %20 %
Elongation · Rod · 0.24 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %18 %
Elongation · Wire · 0.08 · 1/2 Hard (H02) · TYPICAL · 20 °CUnit: %— %6 %
Shear Strength · Rod · 0.25 · 1/2 Hard (H02) · TYPICALUnit: MPa— MPa179.3 MPa
Shear Strength · Rod · 1 · 1/2 Hard (H02) · TYPICALUnit: MPa— MPa172.4 MPa
Shear Strength · Rod · 2 · 1/2 Hard (H02) · TYPICALUnit: MPa— MPa172.4 MPa
Shear Strength · Rod · 0.5 · 1/2 Hard (H02) · TYPICALUnit: MPa— MPa179.3 MPa
Shear Strength · Wire · 0.08 · 1/2 Hard (H02) · TYPICALUnit: MPa— MPa186.2 MPa
5. Electrical & Thermal Conductive Properties
PropertyC63200 Nickel-Aluminum Bronze (Naval Alloy)C14500 Tellurium Copper
Electrical Conductivity · TYPICAL · 20 °CCategory: ELECTRICAL • Unit: % IACS7 % IACS93 % IACS
Liquidus Temperature · TYPICALCategory: THERMAL • Unit: °C1060 °C1080 °C
Solidus Temperature · TYPICALCategory: THERMAL • Unit: °C1040.6 °C1051.1 °C
Thermal Conductivity · TYPICAL · 20 °CCategory: THERMAL • Unit: W/(m·K)34.61 W/(m·K)354.8 W/(m·K)
Coefficient of Thermal Expansion (CTE) · TYPICALCategory: THERMAL • Unit: µm/(m·K)16.2 µm/(m·K)17.1 µm/(m·K)
Coefficient of Thermal Expansion (CTE) · TYPICALCategory: THERMAL • Unit: µm/(m·K)— µm/(m·K)17.46 µm/(m·K)
Coefficient of Thermal Expansion (CTE) · TYPICALCategory: THERMAL • Unit: µm/(m·K)— µm/(m·K)17.82 µm/(m·K)
Specific Heat Capacity · TYPICAL · 20 °CCategory: THERMAL • Unit: J/(kg·K)439.6 J/(kg·K)385.2 J/(kg·K)
Annealing Temperature Range · RANGECategory: THERMAL • Unit: °C621.1–704.4 °C426.7–648.9 °C
Hot Working Temperature Range · RANGECategory: THERMAL • Unit: °C815.6–898.9 °C760–871.1 °C
6. Hardness Evaluation (Discrete Scales Preserved)No cross-scale mathematical conversion
Hardness ScaleC63200 Nickel-Aluminum Bronze (Naval Alloy)C14500 Tellurium Copper
Rockwell B Hardness · Forgings · 5 · Light Anneal (O50) · TYPICAL92 HRB—
Rockwell B Hardness · Plate · 0.5 · Light Anneal (O50) · TYPICAL89 HRB—
Rockwell B Hardness · Plate · 0.25 · Light Anneal (O50) · TYPICAL92 HRB—
Rockwell B Hardness · Plate · 1 · Light Anneal (O50) · TYPICAL85 HRB—
Rockwell B Hardness · Rod · 2 · Light Anneal (O50) · TYPICAL94 HRB—
Rockwell B Hardness · Rod · 1 · Light Anneal (O50) · TYPICAL96 HRB—
Rockwell B Hardness · Rod · 3 · Light Anneal (O50) · TYPICAL93 HRB—
Rockwell B Hardness · Rod · 0.25 · 1/2 Hard (H02) · TYPICAL—43 HRB
Rockwell B Hardness · Rod · 1 · 1/2 Hard (H02) · TYPICAL—42 HRB
Rockwell B Hardness · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL—43 HRB
Rockwell 30T Hardness · Rod · 0.5 · 1/2 Hard (H02) · TYPICAL—50 HR30T
7. Fabrication & Processing Comparison
C63200 Nickel-Aluminum Bronze (Naval Alloy) Characteristics:

Machinability: Machinability rating: 30% relative to free-cutting brass (C36000 = 100%). Forgeability rating: 70.

Weldability: Soldering: Fair; Brazing: Fair; Oxyacetylene Welding: Not Recommended; Gas Shielded Arc Welding: Excellent; Coated Metal Arc Welding: Good; Spot Weld: Good; Seam Weld: Fair; Butt Weld: Good

Formability / Cold Working: Capacity for Being Cold Worked: Fair. Capacity for Being Hot Formed: Good.

Heat Treatment & Annealing: Annealing temperature range: 621.1°C to 704.4°C (1150°F - 1300°F). Hot working temperature range: 815.6°C to 898.9°C (1500°F - 1650°F).

C14500 Tellurium Copper Characteristics:

Machinability: Machinability rating: 85% relative to free-cutting brass (C36000 = 100%). Forgeability rating: 65.

Weldability: Soldering: Excellent; Brazing: Good; Oxyacetylene Welding: Fair; Gas Shielded Arc Welding: Fair; Coated Metal Arc Welding: Not Recommended; Spot Weld: Not Recommended; Seam Weld: Not Recommended; Butt Weld: Fair

Formability / Cold Working: Capacity for Being Cold Worked: Good. Capacity for Being Hot Formed: Good.

Heat Treatment & Annealing: Annealing temperature range: 426.7°C to 648.9°C (800°F - 1200°F). Hot working temperature range: 760.0°C to 871.1°C (1400°F - 1600°F).