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Copper Alloy C62580-M11

Temper

UNS C62580 · ASTM B150

M11 = as forged and quenched

Closed-die or open-die forgings supplied without further heat treatment — used for high-strength fittings and fastener blanks.

High cost $$$$

Values for the M11 condition

Other C62580 tempers and conditions

C62580 is listed in 4 conditions; see the grade overview at C62580.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Softest supply condition for easier machining or before a subsequent hardening cycle; strength and wear resistance are reduced.3507008217 HB—
M11This page
As forged and quenched
Closed-die or open-die forgings supplied without further heat treatment — used for high-strength fittings and fastener blanks.414758622 HRC7.5 % IACS
M30Default
As hot extruded
Standard stocked bar/rod condition: full hot-worked strength with the best elongation this alloy offers.427772522 HRC7.5 % IACS
Quench hardened and temper annealed
Pick for maximum hardness and galling/wear resistance (dies, wear plates, guide blocks); ductility drops to ~2%.545827229 HRC—

What is C62580-M11?

C62580-M11 is C62580 in the M11 temper — closed-die or open-die forgings supplied without further heat treatment — used for high-strength fittings and fastener blanks. C62580-M11 has a yield strength of 414 MPa (60 ksi) and a tensile strength of 758 MPa (110 ksi) — stronger than 81% of copper alloy grades. Elongation at break is 6% and the elastic modulus is 110 GPa (16 Msi). C62580-M11 has a density of 7.25 g/cm³ (0.262 lb/in³), lighter than 100% of copper alloy grades. It melts at 1,027°C (1,881 °F). M30 is the default condition FabDigit quotes; M11 is available on request or by drawing note.

Advantages

  • Lightweight — 7.25 g/cm³ (0.262 lb/in³), better than 100% of copper alloy grades
  • High service temperature — 300°C (572 °F), better than 85% of copper alloy grades
  • High strength — 414 MPa (60 ksi), better than 81% of copper alloy grades

Limitations

  • Limited ductility — 6%, worse than 89% of copper alloy grades
  • Limited formability — 12/100, worse than 85% of copper alloy grades
  • Low electrical conductivity — 7.5 % IACS, worse than 84% of copper alloy grades
  • Poor heat conductor — 42 W/m·K (24.3 BTU/hr·ft·°F), worse than 80% of copper alloy grades

C62580-M11 properties

Typical room-temperature values for C62580-M11; 23 are specific to this condition. Other listed values are C62580 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C62580-M11 has a density of 7.25 g/cm³ (0.262 lb/in³), lighter than 100% of copper alloy grades. It melts at 1,027°C (1,881 °F).

Density7.25 g/cm³0.26 lb/in³
Melting Point (Solidus)1,027°C1,881 °F
Liquidus Temperature1,046°C1,915 °F

Mechanical14

C62580-M11 has a yield strength of 414 MPa (60 ksi) and a tensile strength of 758 MPa (110 ksi) — stronger than 81% of copper alloy grades. Elongation at break is 6% and the elastic modulus is 110 GPa (16 Msi).

Elastic (Young's) Modulus110 GPa16 Msi
Shear Modulus42 GPa6.1 Msi
Bulk Modulus105 GPa15.2 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)758 MPa110 ksi
Yield Strength (0.2% offset)414 MPa60 ksi
Elongation at Break6%
Reduction in Area9%
Shear Strength462 MPa67 ksi
Fatigue Strength (Endurance Limit)245 MPa35.5 ksi
Charpy V-Notch Impact (RT)11 J8.1 ft·lbf
Hardness, Brinell235 HB
Hardness, Rockwell C22 HRC
Hardness, Vickers247 HV

Thermal6

C62580-M11 is rated for continuous service to 300°C (572 °F). It conducts heat at 42 W/m·K (24.3 BTU/hr·ft·°F), worse than 80% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity42 W/m·K24.3 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 Fusion220 J/g94.6 BTU/lb
Max Service Temperature (continuous)300°C572 °F
Min Service Temperature-200°C-328 °F

Electrical3

C62580-M11 conducts electricity at 7.5 % IACS, worse than 84% of copper alloy grades.

Electrical Conductivity7.5 % IACS
Electrical Resistivity2.3×10⁻⁷ Ω·m9.06 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is very good (70/100), better than 76% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.27 V
Corrosion ResistanceVery good70/100
Chemical Resistance SummaryGood resistance to seawater, brines, non-oxidizing acids (dilute H2SO4, HCl at low concentration), organic acids and steam; poor in nitric/oxidizing acids, ammonia and amines (SCC risk); high Al with little Ni makes it susceptible to dealuminification in stagnant hot chlorides.

Sustainability4

Producing a kilogram of C62580-M11 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 Water320 L/kg38.3 gal/lb
Typical Recycled Content35%

Manufacturability8

C62580-M11's machinability is poor (27/100, worse than 81% of copper alloy grades); weldability poor (32/100); formability not recommended (12/100).

MachinabilityPoor27/100
Machinability Rating (AISI 1212 = 100 %)22%
WeldabilityPoor32/100
Formability (cold)Not recommended12/100
CastabilityGood55/100
Brazeability / SolderabilityPoor30/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper-base alloy; use passivation, chemical blackening or electroless nickel instead

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

Working with C62580-M11

Is C62580 easy to machine?

Machine like a hard bronze: rigid setup, sharp carbide (K-grade) tools, 5–8° positive rake, 60–120 m/min, generous flood coolant; chips are short and abrasive — rating only about 20 % of free-cutting brass.

Can C62580 be welded?

GTAW/GMAW with matching Al-bronze filler (ERCuAl-A2/A3), preheat 150–250 °C, tight interpass control and slow cooling; high Al content makes it crack- and oxide-film sensitive, so post-weld temper anneal is recommended.

Can C62580 be formed, bent or molded?

Hot forge/extrude at roughly 750–870 °C; virtually no cold formability — bending or heading at room temperature will crack the eutectoid structure.

What surface finishes work on C62580?

Not anodizable; use vapour degrease plus mechanical polish, chemical blackening, passivation or electroless nickel; the alumina film gives good natural tarnish resistance.

C62580 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
Alhigh-aluminium (β-hardenable) range per ASTM B150; verify against mill certificate12 – 1312.5
Fegrain refiner / κ-phase former3 – 54
Nimax, improves dealuminification resistance≤ 20.5
Mn≤ 20.3
Si≤ 0.1—
Zn≤ 0.1—
Sn≤ 0.2—
Curemainder, approx. 81–84 %balance—

C62580-M11 — frequently asked

What is C62580-M11 used for?

C62580-M11 is typically used for aircraft fasteners, high-strength bolts and forged fittings. In short: high-strength forging bronze; aerospace fastener grade; low ductility, hot work only.

What is the yield strength of C62580-M11?

C62580-M11 has a typical yield strength of 414 MPa (60 ksi) and a tensile strength of 758 MPa (110 ksi) — stronger than 81% of copper alloy grades. Strength varies by condition: see the 4 listed tempers.

Is C62580-M11 easy to machine?

Not especially — machinability is rated poor (27/100, worse than 81% of copper alloy grades). Machine like a hard bronze: rigid setup, sharp carbide (K-grade) tools, 5–8° positive rake, 60–120 m/min, generous flood coolant; chips are short and abrasive — rating only about 20 % of free-cutting brass.

Can C62580-M11 be welded?

Not readily — weldability is rated poor (32/100). GTAW/GMAW with matching Al-bronze filler (ERCuAl-A2/A3), preheat 150–250 °C, tight interpass control and slow cooling; high Al content makes it crack- and oxide-film sensitive, so post-weld temper anneal is recommended.

What surface finishes work on C62580-M11?

Not anodizable; use vapour degrease plus mechanical polish, chemical blackening, passivation or electroless nickel; the alumina film gives good natural tarnish resistance.

Can C62580-M11 be formed, bent or molded?

Hot forge/extrude at roughly 750–870 °C; virtually no cold formability — bending or heading at room temperature will crack the eutectoid structure.

What is the maximum service temperature of C62580-M11?

C62580-M11 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 C62580-M30 and C62580-TQ50?

M30 is the default condition — standard stocked bar/rod condition: full hot-worked strength with the best elongation this alloy offers. TQ50: pick for maximum hardness and galling/wear resistance (dies, wear plates, guide blocks); ductility drops to ~2%. Yield strength is 427 MPa in M30 versus 545 MPa in TQ50.

Sources

  1. ASTM B150/B150M — Aluminum Bronze Rod, Bar and Shapes — ASTM International (2019)
  2. CDA / copper.org alloy datasheets, wrought aluminium bronzes C62xxx — Copper Development Association (2023)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  4. High-aluminium wrought bronze wear-alloy datasheets (AMPCO-class bar/forgings) — AMPCO Metal (2022)

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.