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Copper Alloys•Aluminum Bronze•
VERIFIED

C63000 Nickel-Aluminum Bronze (AMS 4640)

Primary Designation:UNS C63000
Aliases:
Nickel-Aluminum BronzeAMS 4640 alloyC63000

Mat Grades internal verification confirms source-backed fidelity and data integrity. It does not constitute external certification, ASTM/CDA endorsement, or guaranteed material conformity for procurement.

Data Completeness & Record Integrity:8 composition elements and 50 contextual property values cataloged.
Omitted fields represent unverified parameters. "Missing is better than invented."

Key Engineering Properties

Representative source rows, qualified by their reported conditions. Inspect the tables below for all values, limits, and source notes.

Density
7.584 g/cm³TYPICAL · at 20 °C
Electrical Conductivity
7 % IACSTYPICAL · at 20 °C
Thermal Conductivity
39.11 W/(m·K)TYPICAL · at 20 °C
Specific Heat Capacity
376.8 J/(kg·K)TYPICAL · at 20 °C
Melting Range (Solidus / Liquidus)
1035 – 1054.4 °C1895.0 – 1930.0 °F
Solidus: 1035°C | Liquidus: 1054.4°C
Composition Excerpt
Cu BALANCE wt%Copper (balance)
Standard Elemental Basis: BALANCE

Engineering Summary

UNS C63000 Nickel-Aluminum Bronze (9.0-11.0% Al, 4.0-5.5% Ni, 2.0-4.0% Fe) is an ultra-high-strength wrought alloy (AMS 4640 / ASTM B150) heat-treatable to high hardness. Renowned for superior resistance to cavitation erosion, shock loading, and marine corrosion, commonly specified for aircraft landing gear bushings, marine valves, and heavy-duty wear rings.

Documented Product Applications (Cited CDA Reference Profile)

  • ›Aircraft Parts: Friction & Wear Properties
  • ›Aircraft Parts: Impact Resistance
  • ›Aircraft Parts: Mechanical Properties
  • ›Balls: Corrosion Resistance
  • ›Balls: Friction & Wear Properties
  • ›Balls: Mechanical Properties
  • ›Bearings: Corrosion Resistance
  • ›Bearings: Friction & Wear Properties
  • ›Bearings: Mechanical Properties
  • ›Bolts: Corrosion Resistance
  • ›Bolts: Impact Resistance
  • ›Bolts: Mechanical Properties

Recognized Aliases

Source-backed commercial trade name and short designations cataloged in canonical data.

Nickel-Aluminum BronzeAMS 4640 alloyC63000

Standard Designations & Applicable Specifications

Semantically classified designations distinguishing primary standard identifiers, commercial trade names, and applicable specification references.

Direct Standard DesignationsDIRECT DESIGNATION
2 Primary Identifiers
SystemIdentifierStandard System NameClassification Notes & Provenance
UNSPRIMARYC63000Unified Numbering SystemUnified Numbering System standard designation for copper alloys (CDA / SAE / ASTM)Ref: CDA UNS Standard Designations Register (C63000)
CDAAlloy 630Copper Development Association Alloy NumberCDA three-digit legacy designationRef: CDA UNS Standard Designations Register (C63000)
Recognized Commercial Aliases & Trade NamesCOMMON ALIAS
4 Listed
Recognized Name / AliasClassificationTechnical Usage & Context
Nickel-Aluminum Bronze (AMS 4640)Standard Commercial NameCDA Standard Commercial Name
Nickel-Aluminum BronzeCommercial AliasColloquial or commercial industry synonym
AMS 4640 alloyCommercial AliasColloquial or commercial industry synonym
C63000Commercial AliasColloquial or commercial industry synonym
Applicable Specifications & Product Form ReferencesSPECIFICATION REFERENCE
12 Applicable Standards
Standards BodySpecification CodeSpecification Title / ScopeRelationship Type
SAESAE J461WROUGHT AND CAST COPPER ALLOYSSpecification Reference
SAESAE J463WROUGHT COPPER AND COPPER ALLOYSSpecification Reference
ASTMASTM B124/B124MCOPPER AND COPPER-ALLOY FORGING ROD, BAR AND SHAPESSpecification Reference
AMSAMS 4640ALUMINUM BRONZE BARS, RODS, SHAPES, TUBES, AND FORGINGSSpecification Reference
FEDERALFEDERAL QQ-C-450COPPER-ALUMINUM ALLOY (ALUMINUM BRONZE, PLATE, SHEET, STRIP, AND BAR)Specification Reference
ASTMASTM F468NONFERROUS BOLTS, HEX CAP SCREWS, AND STUDS FOR GENERAL USESpecification Reference
MILITARYMILITARY MIL-B-16166BRONZE, ALUMINUM, FORGINGS, HEAT TREATEDSpecification Reference
ASMEASME SB283COPPER AND COPPER ALLOY DIE FORGINGS (HOT PRESSED)Specification Reference
ASTMASTM B283/B283MCOPPER AND COPPER ALLOY DIE FORGINGS (HOT PRESSED)Specification Reference
ASTMASTM F467NONFERROUS NUTS FOR GENERAL USESpecification Reference
ASTMASTM B171/B171MCOPPER ALLOY CONDENSER TUBE PLATESSpecification Reference
ASMEASME SB171COPPER ALLOY CONDENSER TUBE PLATESSpecification Reference
Engineering Notice: Applicable specifications establish manufacturing requirements, dimensional tolerances, and test criteria for specific product forms (e.g. bus bar, wire, plate, pipe). They represent applicable technical standards, not alternative or equivalent alloy grades.

Chemical Composition (Weight %)

Elemental limits and values from the cited source. Preserves exact semantic limits (minimums, maximums, and ranges).

ElementSymbolAtomic No.Semantic BasisSpecified ValueUnitMetallurgical Notes & QualificationData Status
CopperCu29BALANCEBalancewt%Remainder element (Copper).Ref: Copper Development Association (CDA)VERIFIED
TinSn50MAXIMUM≤ 0.20wt%CDA chemical composition specification limits for C63000: max 0.2 wt%.Ref: Copper Development Association (CDA)VERIFIED
ZincZn30MAXIMUM≤ 0.30wt%CDA chemical composition specification limits for C63000: max 0.3 wt%.Ref: Copper Development Association (CDA)VERIFIED
IronFe26RANGE2.00 – 4.00wt%CDA chemical composition specification limits for C63000: 2.0 - 4.0 wt%.Ref: Copper Development Association (CDA)VERIFIED
NickelNi28RANGE4.00 – 5.50wt%CDA chemical composition specification limits for C63000: 4.0 - 5.5 wt%.Ref: Copper Development Association (CDA)VERIFIED
AluminumAl13RANGE9.00 – 11.00wt%CDA chemical composition specification limits for C63000: 9.0 - 11.0 wt%.Ref: Copper Development Association (CDA)VERIFIED
ManganeseMn25MAXIMUM≤ 1.50wt%CDA chemical composition specification limits for C63000: max 1.5 wt%.Ref: Copper Development Association (CDA)VERIFIED
SiliconSi14MAXIMUM≤ 0.25wt%CDA chemical composition specification limits for C63000: max 0.25 wt%.Ref: Copper Development Association (CDA)VERIFIED
* Elemental percentages are expressed in weight percent (wt%). Values represent applicable specification limits. Unspecified trace elements are not fabricated or assumed.Preserves exact semantic basis
Property Display UnitsSwitch between Canonical SI and Source / US Customary units:

Physical Properties

Source-specific physical properties. Test temperatures are shown only where reported.

1 Parameters
Property ParameterCanonical SI ValueSemantic BasisTest Temperature / Context RangeSource Raw ReferenceSource ReferenceStatus
Density7.584 g/cm³TYPICALTest Temp: 20 °CCDA Physical Properties: Density 0.274 lb/cu in. at 68°F (7.584 g/cm³ at 20°C)0.274 lb/cu in. at 68°FCopper Development Association Inc.VERIFIED

Thermal & Thermodynamic Properties

Phase change temperatures, thermal conductivity, specific heat, mean coefficients of thermal expansion across standardized temperature ranges, and recommended thermal processing windows.

7 Parameters
Property ParameterCanonical SI ValueSemantic BasisTest Temperature / Context RangeSource Raw ReferenceSource ReferenceStatus
Liquidus Temperature1054.4 °CTYPICALCDA Physical Properties: Liquidus temperature 1930.0 °F (1054.4 °C)1930.0 °FCopper Development Association Inc.VERIFIED
Solidus Temperature1035 °CTYPICALCDA Physical Properties: Solidus temperature 1895.0 °F (1035.0 °C)1895.0 °FCopper Development Association Inc.VERIFIED
Thermal Conductivity39.11 W/(m·K)TYPICALTest Temp: 20 °CCDA Physical Properties: Thermal conductivity 22.6 Btu/(ft·hr·°F) (39.11 W/(m·K) at 20°C)22.6 Btu/ sq ft/ ft hr/ °F at 68°FCopper Development Association Inc.VERIFIED
Coefficient of Thermal Expansion (CTE)16.2 µm/(m·K)TYPICALCDA Physical Properties: CTE 9.0 µin/(in·°F) (16.2 µm/(m·K)) over range 68-57210°F9.0 10^-6 per °FCopper Development Association Inc.VERIFIED
Specific Heat Capacity376.8 J/(kg·K)TYPICALTest Temp: 20 °CCDA Physical Properties: Specific heat 0.09 Btu/(lb·°F) (376.8 J/(kg·K))0.09 Btu/ lb /°F at 68°FCopper Development Association Inc.VERIFIED
Annealing Temperature Range593.3 – 704.4 °CRANGECDA Thermal Treatments: Annealing temperature range 1100 - 1300°F (593.3 - 704.4°C)1100 – 1300 °FCopper Development Association Inc.VERIFIED
Hot Working Temperature Range787.8 – 926.7 °CRANGECDA Thermal Treatments: Hot working range 1450 - 1700°F (787.8 - 926.7°C)1450 – 1700 °FCopper Development Association Inc.VERIFIED

Electrical Properties

Electrical conductivity and resistivity in their reported units and conditions.

1 Parameters
Property ParameterCanonical SI ValueSemantic BasisTest Temperature / Context RangeSource Raw ReferenceSource ReferenceStatus
Electrical Conductivity7 % IACSTYPICALTest Temp: 20 °CCDA Physical Properties: Volume conductivity 7.0 % IACS at 68°F (20°C)7.0 % IACS at 68°FCopper Development Association Inc.VERIFIED

Contextual Mechanical Properties & Tempers

Engineering strength, ductility, and hardness values grouped by product form, temper, and section thickness. Mechanical properties are contextual and not isotropic averages.

Elastic & Baseline Mechanical ConstantsSource-specific measurement conditions
Modulus of Elasticity (Tension)
120.7 GPa
CDA Physical Properties: Elastic modulus in tension 17500.0 ksi (120.7 GPa)
Modulus of Rigidity
44126.4 MPa
CDA Physical Properties: Shear modulus 6400.0 ksi (44126.4 MPa)
Machinability Rating
30 %
CDA Fabrication Properties: Rating relative to Free-Cutting Brass (C36000 = 100%).
Forgeability Rating
75 —
CDA Fabrication Properties: Relative forgeability rating.
Showing 14 of 14 conditions
Product FormTemper / ConditionSection SizeTensile (UTS)Yield StrengthElongationShear StrengthFatigue StrengthHardness (Scales Preserved)Status
BarAs Hot Extruded (M30) · 20 °C
Source values and qualifiers
Tensile Strength: 620.5 MPa (TYPICAL)Section Size: 3; Section Size: 3 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 344.7 MPa (TYPICAL)Section Size: 3; Section Size: 3 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 15 % (TYPICAL)Section Size: 3; Section Size: 3 inCopper Development Association (CDA) —
M30
3620.5 MPa344.7 MPa15 %———VERIFIED
BarAs Hot Extruded (M30)
Source values and qualifiers
Rockwell B Hardness: 96 HRB (TYPICAL)Section Size: 3; Section Size: 3 inCopper Development Association (CDA) —
M30
3—————
96 HRB
VERIFIED
BarDrawn and Stress Relieved (HR50) · 20 °C
Source values and qualifiers
Tensile Strength: 689.5 MPa (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 413.7 MPa (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 15 % (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
HR50
2689.5 MPa413.7 MPa15 %———VERIFIED
BarDrawn and Stress Relieved (HR50)
Source values and qualifiers
Rockwell B Hardness: 96 HRB (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
HR50
2—————
96 HRB
VERIFIED
BarDrawn and Stress Relieved (HR50) · 20 °C
Source values and qualifiers
Tensile Strength: 758.4 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 427.5 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 15 % (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
HR50
1758.4 MPa427.5 MPa15 %———VERIFIED
BarDrawn and Stress Relieved (HR50)
Source values and qualifiers
Rockwell B Hardness: 97 HRB (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
Fatigue Strength: 255.1 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 in; 10^8 cycles endurance limitCopper Development Association (CDA) —
HR50
1————255.1 MPa
97 HRB
VERIFIED
RodAs Hot Extruded (M30) · 20 °C
Source values and qualifiers
Tensile Strength: 689.5 MPa (TYPICAL)Section Size: 4; Section Size: 4 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 413.7 MPa (TYPICAL)Section Size: 4; Section Size: 4 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 15 % (TYPICAL)Section Size: 4; Section Size: 4 inCopper Development Association (CDA) —
M30
4689.5 MPa413.7 MPa15 %———VERIFIED
RodAs Hot Extruded (M30)
Source values and qualifiers
Rockwell B Hardness: 96 HRB (TYPICAL)Section Size: 4; Section Size: 4 inCopper Development Association (CDA) —
Shear Strength: 427.5 MPa (TYPICAL)Section Size: 4; Section Size: 4 inCopper Development Association (CDA) —
Fatigue Strength: 248.2 MPa (TYPICAL)Section Size: 4; Section Size: 4 in; 10^8 cycles endurance limitCopper Development Association (CDA) —
M30
4———427.5 MPa248.2 MPa
96 HRB
VERIFIED
RodDrawn and Stress Relieved (HR50) · 20 °C
Source values and qualifiers
Tensile Strength: 813.6 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 517.1 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 15 % (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
HR50
1813.6 MPa517.1 MPa15 %———VERIFIED
RodDrawn and Stress Relieved (HR50)
Source values and qualifiers
Rockwell B Hardness: 98 HRB (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
Shear Strength: 482.6 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 inCopper Development Association (CDA) —
Fatigue Strength: 255.1 MPa (TYPICAL)Section Size: 1; Cold Work: 10%; Section Size: 1 in; 10^8 cycles endurance limitCopper Development Association (CDA) —
HR50
1———482.6 MPa255.1 MPa
98 HRB
VERIFIED
RodDrawn and Stress Relieved (HR50) · 20 °C
Source values and qualifiers
Tensile Strength: 792.9 MPa (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 448.2 MPa (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 18 % (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
HR50
2792.9 MPa448.2 MPa18 %———VERIFIED
RodDrawn and Stress Relieved (HR50)
Source values and qualifiers
Rockwell B Hardness: 96 HRB (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
Shear Strength: 475.7 MPa (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 inCopper Development Association (CDA) —
Fatigue Strength: 262 MPa (TYPICAL)Section Size: 2; Cold Work: 10%; Section Size: 2 in; 10^8 cycles endurance limitCopper Development Association (CDA) —
HR50
2———475.7 MPa262 MPa
96 HRB
VERIFIED
RodDrawn and Stress Relieved (HR50) · 20 °C
Source values and qualifiers
Tensile Strength: 772.2 MPa (TYPICAL)Section Size: 3; Cold Work: 10%; Section Size: 3 inCopper Development Association (CDA) —
Yield Strength (0.5% Ext): 427.5 MPa (TYPICAL)Section Size: 3; Cold Work: 10%; Section Size: 3 in; Yield strength at 0.5% extension under loadCopper Development Association (CDA) —
Elongation: 20 % (TYPICAL)Section Size: 3; Cold Work: 10%; Section Size: 3 inCopper Development Association (CDA) —
HR50
3772.2 MPa427.5 MPa20 %———VERIFIED
RodDrawn and Stress Relieved (HR50)
Source values and qualifiers
Rockwell B Hardness: 96 HRB (TYPICAL)Section Size: 3; Cold Work: 10%; Section Size: 3 inCopper Development Association (CDA) —
Shear Strength: 448.2 MPa (TYPICAL)Section Size: 3; Cold Work: 10%; Section Size: 3 inCopper Development Association (CDA) —
Fatigue Strength: 255.1 MPa (TYPICAL)Section Size: 3; Cold Work: 10%; Section Size: 3 in; 10^8 cycles endurance limitCopper Development Association (CDA) —
HR50
3———448.2 MPa255.1 MPa
96 HRB
VERIFIED
Hardness Integrity Notice: Rockwell B (HRB), Rockwell F (HRF), and Superficial 30T (HR30T) scales are reported on their measured scales without cross-scale mathematical conversion.
Source: See fact-level citations

Processing & Fabrication Characteristics

Machining, joining, forming, and thermal processing ratings cataloged from the cited authoritative technical reference.

Source: Copper Development Association (CDA)

Machinability

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

Weldability & Joining

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

Heat Treatment & Working Ranges

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).

Forming & Cold Working

Capacity for Being Cold Worked: Poor. Capacity for Being Hot Formed: Good.

Comparable Grades & Cross-References

Carefully classified cross-reference relationships for C63000 Nickel-Aluminum Bronze (AMS 4640). Comparable does not mean equivalent.

Related MaterialFamilyRelationship ClassificationMetallurgical Notes & DifferencesStatusAction
C95400 Aluminum Bronze 9CCopper AlloysCommonly ComparedC63000 is wrought nickel-aluminum bronze (AMS 4640 / ASTM B150) providing void-free metallurgical density and higher fatigue strength; C95400 is continuous-cast aluminum bronze (Alloy 9C).Materials serve different design priorities (e.g. higher strength vs superior corrosion resistance or cost).VERIFIEDSide-by-Side Compare →
C63200 Nickel-Aluminum Bronze (Naval Alloy)Copper AlloysCommonly ComparedC63000 (AMS 4640) and C63200 (MIL-B-24480) are wrought nickel-aluminum bronzes; C63200 strictly restricts iron content below nickel and tightens manganese limits to ensure high dynamic fracture toughness for naval submarine service. Qualification cannot be inferred from specification name.Materials serve different design priorities (e.g. higher strength vs superior corrosion resistance or cost).VERIFIEDSide-by-Side Compare →

Sources & Provenance Trail

Reference publications and standards organization registers cited across this material record.

Copper Development Association Inc.CDA Alloy C63000 Property & Specification Profile
AUTHORITATIVE BODY

Copper Development Association authoritative technical reference profile for C63000 Nickel-Aluminum Bronze (AMS 4640).

Issuing Body: Copper Development Association (CDA)View Source Record ↗
Copper Development Association Inc.CDA UNS Standard Designations Register (C63000)
AUTHORITATIVE BODY

Unified Numbering System (UNS) designation registration register confirming active C63000 status.

Issuing Body: Copper Development Association (CDA)View Source Record ↗
Intellectual Property & Provenance Notice: Mat Grades cites technical literature from recognized industry associations and standards organizations. Underlying technical standards and publication data remain the intellectual property of their respective issuing organizations.