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Material Comparison Engine

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

Material A (Baseline)
Material B (Comparison)
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Temper & Metallurgical Context Qualification:The selected records contain different or missing source contexts. Values shown in separate rows are not directly matched. Typical and estimated values are not guaranteed minima; matching context alone does not establish interchangeability.
1. Identity, Classification & Standards
ParameterC63000 Nickel-Aluminum Bronze (AMS 4640)C63200 Nickel-Aluminum Bronze (Naval Alloy)
Material FamilyCopper AlloysCopper Alloys
SubfamilyAluminum BronzeAluminum Bronze
UNS DesignationC63000C63200
COMMERCIAL DesignationNickel-Aluminum Bronze (AMS 4640)Nickel-Aluminum Bronze (Naval Alloy)
CDA DesignationAlloy 630Alloy 632
SPECIFICATION DesignationSAE J461ASTM B124/B124M
2. Chemical Composition Limits (wt %)Source-specific limits and typical values
ElementC63000 Nickel-Aluminum Bronze (AMS 4640)C63200 Nickel-Aluminum Bronze (Naval Alloy)
Cu (Copper)Bal.Bal.
Sn (Tin)≤ 0.2%—
Zn (Zinc)≤ 0.3%—
Fe (Iron)2 – 4%3.5 – 4.3%
Ni (Nickel)4 – 5.5%4 – 4.8%
Al (Aluminum)9 – 11%8.7 – 9.5%
Mn (Manganese)≤ 1.5%1.2 – 2%
Si (Silicon)≤ 0.25%≤ 0.1%
Pb (Lead)—≤ 0.02%
3. Physical Properties
PropertyC63000 Nickel-Aluminum Bronze (AMS 4640)C63200 Nickel-Aluminum Bronze (Naval Alloy)
Density · TYPICAL · 20 °CUnit: g/cm³7.584 g/cm³7.64 g/cm³
4. Contextual Mechanical PropertiesUnit: SI
Mechanical ParameterC63000 Nickel-Aluminum Bronze (AMS 4640)As Hot Extruded (M30)C63200 Nickel-Aluminum Bronze (Naval Alloy)Light Anneal (O50)
Modulus of Elasticity (Tension) · TYPICALUnit: GPa120.7 GPa117.2 GPa
Modulus of Rigidity · TYPICALUnit: MPa44126.4 MPa44126.4 MPa
Machinability Rating · TYPICALUnit: %30 %30 %
Forgeability Rating · TYPICALUnit: —75 —70 —
Tensile Strength · Bar · 3 · As Hot Extruded (M30) · TYPICAL · 20 °CUnit: MPa620.5 MPa— MPa
Tensile Strength · Rod · 4 · As Hot Extruded (M30) · TYPICAL · 20 °CUnit: MPa689.5 MPa— MPa
Tensile Strength · Forgings · 5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa689.5 MPa
Tensile Strength · Plate · 0.5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa655 MPa
Tensile Strength · Plate · 0.25 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa689.5 MPa
Tensile Strength · Plate · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa620.5 MPa
Tensile Strength · Rod · 2 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa710.2 MPa
Tensile Strength · Rod · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa723.9 MPa
Tensile Strength · Rod · 3 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa703.3 MPa
Yield Strength (0.5% Ext) · Bar · 3 · As Hot Extruded (M30) · TYPICAL · 20 °CUnit: MPa344.7 MPa— MPa
Yield Strength (0.5% Ext) · Rod · 4 · As Hot Extruded (M30) · TYPICAL · 20 °CUnit: MPa413.7 MPa— MPa
Yield Strength (0.5% Ext) · Forgings · 5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa310.3 MPa
Yield Strength (0.5% Ext) · Plate · 0.5 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa324.1 MPa
Yield Strength (0.5% Ext) · Plate · 0.25 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa344.7 MPa
Yield Strength (0.5% Ext) · Plate · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa310.3 MPa
Yield Strength (0.5% Ext) · Rod · 2 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa358.5 MPa
Yield Strength (0.5% Ext) · Rod · 1 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa365.4 MPa
Yield Strength (0.5% Ext) · Rod · 3 · Light Anneal (O50) · TYPICAL · 20 °CUnit: MPa— MPa351.6 MPa
Elongation · Bar · 3 · As Hot Extruded (M30) · TYPICAL · 20 °CUnit: %15 %— %
Elongation · Rod · 4 · As Hot Extruded (M30) · TYPICAL · 20 °CUnit: %15 %— %
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 %
Fatigue Strength · Rod · 4 · As Hot Extruded (M30) · TYPICALUnit: MPa248.2 MPa— MPa
Shear Strength · Rod · 4 · As Hot Extruded (M30) · TYPICALUnit: MPa427.5 MPa— MPa
5. Electrical & Thermal Conductive Properties
PropertyC63000 Nickel-Aluminum Bronze (AMS 4640)C63200 Nickel-Aluminum Bronze (Naval Alloy)
Electrical Conductivity · TYPICAL · 20 °CCategory: ELECTRICAL • Unit: % IACS7 % IACS7 % IACS
Liquidus Temperature · TYPICALCategory: THERMAL • Unit: °C1054.4 °C1060 °C
Solidus Temperature · TYPICALCategory: THERMAL • Unit: °C1035 °C1040.6 °C
Thermal Conductivity · TYPICAL · 20 °CCategory: THERMAL • Unit: W/(m·K)39.11 W/(m·K)34.61 W/(m·K)
Coefficient of Thermal Expansion (CTE) · TYPICALCategory: THERMAL • Unit: µm/(m·K)16.2 µm/(m·K)16.2 µm/(m·K)
Specific Heat Capacity · TYPICAL · 20 °CCategory: THERMAL • Unit: J/(kg·K)376.8 J/(kg·K)439.6 J/(kg·K)
Annealing Temperature Range · RANGECategory: THERMAL • Unit: °C593.3–704.4 °C621.1–704.4 °C
Hot Working Temperature Range · RANGECategory: THERMAL • Unit: °C787.8–926.7 °C815.6–898.9 °C
6. Hardness Evaluation (Discrete Scales Preserved)No cross-scale mathematical conversion
Hardness ScaleC63000 Nickel-Aluminum Bronze (AMS 4640)C63200 Nickel-Aluminum Bronze (Naval Alloy)
Rockwell B Hardness · Bar · 3 · As Hot Extruded (M30) · TYPICAL96 HRB—
Rockwell B Hardness · Rod · 4 · As Hot Extruded (M30) · TYPICAL96 HRB—
Rockwell B Hardness · Forgings · 5 · Light Anneal (O50) · TYPICAL—92 HRB
Rockwell B Hardness · Plate · 0.5 · Light Anneal (O50) · TYPICAL—89 HRB
Rockwell B Hardness · Plate · 0.25 · Light Anneal (O50) · TYPICAL—92 HRB
Rockwell B Hardness · Plate · 1 · Light Anneal (O50) · TYPICAL—85 HRB
Rockwell B Hardness · Rod · 2 · Light Anneal (O50) · TYPICAL—94 HRB
Rockwell B Hardness · Rod · 1 · Light Anneal (O50) · TYPICAL—96 HRB
Rockwell B Hardness · Rod · 3 · Light Anneal (O50) · TYPICAL—93 HRB
7. Fabrication & Processing Comparison
C63000 Nickel-Aluminum Bronze (AMS 4640) Characteristics:

Machinability: Machinability rating: 30% relative to free-cutting brass (C36000 = 100%). Forgeability rating: 75.

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

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

Heat Treatment & Annealing: Annealing temperature range: 593.3°C to 704.4°C (1100°F - 1300°F). Hot working temperature range: 787.8°C to 926.7°C (1450°F - 1700°F).

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).