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Copper Alloy C63000-M10

Heat-treated state

UNS C63000 · ASTM B150 · EN CW307G, CuAl10Ni5Fe4 · GB QAl10-4-4

M10 = as hot forged and air cooled

Nickel-aluminium bronze forged to shape and air cooled from the hot-working temperature; retains a fine worked structure with high strength and good toughness.

CNC machiningSheet metalSpecialty cost $$$$$

Values for the M10 condition

Other C63000 tempers and conditions

C63000 is listed in 8 conditions; see the grade overview at C63000.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Softened condition (slow-cooled anneal) used for maximum ductility before further hot/cold forming or machining of complex parts.31065525150 HB7.2 % IACS
Hot rolled and annealed
Hot-rolled plate/bar fully annealed for maximum ductility and lowest residual stress at somewhat reduced strength.32565520170 HB7 % IACS
Hot Extruded and Temper Annealed
Extruded nickel-aluminium bronze given a temper (sub-critical) anneal to stabilise the structure and relieve residual stress with only slight strength loss.34067018180 HB7 % IACS
As hot extruded
Cheapest as-supplied condition for large sections and forging stock where only nominal strength is required.34569020170 HB7 % IACS
M10This page
As hot forged and air cooled
Nickel-aluminium bronze forged to shape and air cooled from the hot-working temperature; retains a fine worked structure with high strength and good toughness.38069013197 HB7 % IACS
HR50Default
Hot rolled / hot finished to specified hardness
Standard stocked condition for ASTM B150 / AMS 4640 nickel-aluminium bronze rod, bar and shapes for marine shafting and valve stems.41576015197 HB7 % IACS
Quench hardened and temper annealed
Choose when maximum and most uniform strength/hardness through heavy sections is needed (heavy forgings, landing-gear bushings, high-load stems).48582512212 HB—
Full hard
Small-diameter cold-drawn rod and wire where higher yield strength and better surface/straightness are wanted; ductility is reduced.5508301019 HRC6.5 % IACS

What is C63000-M10?

C63000-M10 is C63000 heat treated to M10 — nickel-aluminium bronze forged to shape and air cooled from the hot-working temperature; retains a fine worked structure with high strength and good toughness. C63000-M10 has a yield strength of 380 MPa (55.1 ksi) and a tensile strength of 690 MPa (100 ksi) — stronger than 77% of copper alloy grades. Elongation at break is 13% and the elastic modulus is 117 GPa (17 Msi). C63000-M10 has a density of 7.58 g/cm³ (0.274 lb/in³), lighter than 94% of copper alloy grades. It melts at 1,040°C (1,904 °F). HR50 is the default condition FabDigit quotes; M10 is available on request or by drawing note.

Advantages

  • Lightweight — 7.58 g/cm³ (0.274 lb/in³), better than 94% of copper alloy grades
  • Good corrosion resistance — 78/100, better than 94% of copper alloy grades
  • High service temperature — 300°C (572 °F), better than 85% of copper alloy grades
  • Readily welded — 65/100, better than 80% of copper alloy grades
  • High strength — 380 MPa (55.1 ksi), better than 77% of copper alloy grades

Limitations

  • Low electrical conductivity — 7 % IACS, worse than 86% of copper alloy grades
  • Poor heat conductor — 39 W/m·K (22.5 BTU/hr·ft·°F), worse than 83% of copper alloy grades

C63000-M10 properties

Typical room-temperature values for C63000-M10; 39 are specific to this condition. Other listed values are C63000 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C63000-M10 has a density of 7.58 g/cm³ (0.274 lb/in³), lighter than 94% of copper alloy grades. It melts at 1,040°C (1,904 °F).

Density7.58 g/cm³0.27 lb/in³
Melting Point (Solidus)1,040°C1,904 °F
Liquidus Temperature1,054°C1,929 °F

Mechanical14

C63000-M10 has a yield strength of 380 MPa (55.1 ksi) and a tensile strength of 690 MPa (100 ksi) — stronger than 77% of copper alloy grades. Elongation at break is 13% and the elastic modulus is 117 GPa (17 Msi).

Elastic (Young's) Modulus117 GPa17 Msi
Shear Modulus44 GPa6.4 Msi
Bulk Modulus110 GPa16 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)690 MPa100 ksi
Yield Strength (0.2% offset)380 MPa55.1 ksi
Elongation at Break13%
Reduction in Area20%
Shear Strength420 MPa60.9 ksi
Fatigue Strength (Endurance Limit)250 MPa36.3 ksi
Fracture Toughness (K_IC)45 MPa·√m41 ksi·√in
Charpy V-Notch Impact (RT)24 J17.7 ft·lbf
Hardness, Brinell197 HB
Hardness, Rockwell B93 HRB

Thermal6

C63000-M10 is rated for continuous service to 300°C (572 °F). It conducts heat at 39 W/m·K (22.5 BTU/hr·ft·°F), worse than 83% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity39 W/m·K22.5 BTU/hr·ft·°F
Specific Heat Capacity375 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.2 µm/m·K9 µin/in·°F
Latent Heat of Fusion210 J/g90.3 BTU/lb
Max Service Temperature (continuous)300°C572 °F
Min Service Temperature-200°C-328 °F

Electrical3

C63000-M10 conducts electricity at 7 % IACS, worse than 86% of copper alloy grades.

Electrical Conductivity7 % IACS
Electrical Resistivity2.46×10⁻⁷ Ω·m9.69 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is very good (78/100), better than 94% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.25 V
Corrosion ResistanceVery good78/100
Chemical Resistance SummaryExcellent in seawater, brine and mildly acidic media thanks to a tenacious alumina-rich film; attacked by oxidising acids, ammonia and strong alkalis.

Sustainability4

Producing a kilogram of C63000-M10 takes about 58 MJ of energy and emits 3.8 kg of CO₂ — more than 61% of copper alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)58 MJ/kg24,936 BTU/lb
Embodied Carbon (primary production)3.8 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content35%

Manufacturability7

C63000-M10's machinability is poor (30/100, worse than 67% of copper alloy grades); weldability good (65/100); formability poor (30/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)30%
WeldabilityGood65/100
Formability (cold)Poor30/100
Brazeability / SolderabilityPoor30/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper alloy; use passivation/oil or chemical patination instead

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with C63000-M10

Is C63000 easy to machine?

Machines like a tough duplex material: rigid setups, sharp carbide with positive rake, 60–120 m/min, heavy feed and flood coolant to avoid work hardening and gummy chips (rating ≈30% of free-cutting brass).

Can C63000 be welded?

GTAW/GMAW with matching C63000/NAB filler works well; preheat 150–250 °C for heavy sections, avoid excessive heat input and interpass oxide entrapment, no post-weld quench required.

Can C63000 be formed, bent or molded?

Hot work 700–900 °C (excellent forgeability); cold forming is poor — limit to gentle bends with generous radii and interstage annealing.

What surface finishes work on C63000?

Not anodisable; use fine polishing, shot blasting or chemical patination, and avoid electroplating unless a nickel strike is applied over the Al-oxide film.

C63000 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Al9 – 1110
NiNi + Co4 – 5.54.8
Fe2 – 43
Mn≤ 1.50.8
Si≤ 0.25
Zn≤ 0.3
Sn≤ 0.2
Pb≤ 0.02
Curemainder, 78% min≥ 78 (balance)

C63000-M10 — frequently asked

What is C63000-M10 used for?

C63000-M10 is typically used for marine propeller shafting, valve stems, pump sleeves and bushings, aircraft landing-gear bushings, aircraft bearings and heavy-duty gears. In short: extremely tough bronze.

What is the yield strength of C63000-M10?

C63000-M10 has a typical yield strength of 380 MPa (55.1 ksi) and a tensile strength of 690 MPa (100 ksi) — stronger than 77% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C63000-M10 easy to machine?

Not especially — machinability is rated poor (30/100, worse than 67% of copper alloy grades). Machines like a tough duplex material: rigid setups, sharp carbide with positive rake, 60–120 m/min, heavy feed and flood coolant to avoid work hardening and gummy chips (rating ≈30% of free-cutting brass).

Can C63000-M10 be welded?

Yes — weldability is rated good (65/100). GTAW/GMAW with matching C63000/NAB filler works well; preheat 150–250 °C for heavy sections, avoid excessive heat input and interpass oxide entrapment, no post-weld quench required.

What surface finishes work on C63000-M10?

Not anodisable; use fine polishing, shot blasting or chemical patination, and avoid electroplating unless a nickel strike is applied over the Al-oxide film.

Can C63000-M10 be formed, bent or molded?

Hot work 700–900 °C (excellent forgeability); cold forming is poor — limit to gentle bends with generous radii and interstage annealing.

What is the maximum service temperature of C63000-M10?

C63000-M10 is rated for continuous use to about 300°C (572 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C63000-HR50 and C63000-H04?

HR50 is the default condition — standard stocked condition for ASTM B150 / AMS 4640 nickel-aluminium bronze rod, bar and shapes for marine shafting and valve stems. H04: small-diameter cold-drawn rod and wire where higher yield strength and better surface/straightness are wanted; ductility is reduced. Yield strength is 415 MPa in HR50 versus 550 MPa in H04.

Can FabDigit make parts in C63000-M10?

Yes — C63000-M10 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. ASTM B150/B150M — Aluminum Bronze Rod, Bar and Shapes — ASTM (2019)
  2. AMS 4640 — Nickel-Aluminum Bronze Bar, Rod, Shapes, Forgings — SAE International (2018)
  3. ASTM B601 — Temper Designations for Copper and Copper Alloys — ASTM (2019)
  4. CDA Alloy Datasheet C63000 (copper.org) — Copper Development Association (2023)
  5. ASM Handbook Vol.2 — Properties of Nonferrous Alloys — ASM International (1990)
  6. ASM Handbook Vol.13C — Corrosion: Environments and Industries — ASM International (2006)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.