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Copper Alloy C19100-M11

Temper

UNS C19100

M11 = as forged and quenched

Softest, most formable supply condition — Ni-P held in solution so the part can be coined/bent and then aged to full strength.

High cost $$$$

Values for the M11 condition

Other C19100 tempers and conditions

C19100 is listed in 8 conditions; see the grade overview at C19100.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed to 0.050 mm grain size
Fully soft annealed rod/wire for maximum ductility before heading, upsetting or deep bending.1052754065 HB46 % IACS
M11This page
As forged and quenched
Softest, most formable supply condition — Ni-P held in solution so the part can be coined/bent and then aged to full strength.1403103572 HB35 % IACS
As hot forged and air cooled
Standard delivery state of forgings and extrusions where partial in-process ageing gives a useful strength/conductivity balance without extra heat treatment.2153502590 HB42 % IACS
Quarter hard, drawn and stress relieved
Usual screw-machine rod condition: straight, low-residual-stress bar with mid-range strength and clean chip breaking.34041516120 HB44 % IACS
Half hard
Cold-drawn bar/wire when higher strength is wanted without an ageing cycle.38045012130 HB43 % IACS
TF00Default
Solution heat treated and precipitation hardened
Pick for maximum strength plus recovered conductivity and best softening resistance in machined electrical parts.40047015140 HB45 % IACS
Full hard
Highest as-drawn strength and stiffness for pins, studs and spring-loaded contact stems; limited bending.4505008150 HB42 % IACS
TD04 and precipitation hardened
Maximum available strength: hard drawing followed by ageing, for highly loaded machined electrical hardware.5005508165 HB44 % IACS

What is C19100-M11?

C19100-M11 is C19100 in the M11 temper — softest, most formable supply condition — Ni-P held in solution so the part can be coined/bent and then aged to full strength. C19100-M11 has a yield strength of 140 MPa (20.3 ksi) and a tensile strength of 310 MPa (45 ksi) — weaker than 74% of copper alloy grades. Elongation at break is 35% and the elastic modulus is 121 GPa (17.5 Msi). C19100-M11 has a density of 8.86 g/cm³ (0.32 lb/in³), heavier than 68% of copper alloy grades. It melts at 1,035°C (1,895 °F). TF00 is the default condition FabDigit quotes; M11 is available on request or by drawing note.

Advantages

  • Easy to machine — 82/100, better than 90% of copper alloy grades
  • Ductile — tolerates forming and impact — 35%, better than 80% of copper alloy grades
  • Forms and bends easily — 65/100, better than 78% of copper alloy grades

Limitations

  • Difficult to weld — 25/100, worse than 78% of copper alloy grades

C19100-M11 properties

Typical room-temperature values for C19100-M11; 10 are specific to this condition. Other listed values are C19100 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C19100-M11 has a density of 8.86 g/cm³ (0.32 lb/in³), heavier than 68% of copper alloy grades. It melts at 1,035°C (1,895 °F).

Density8.86 g/cm³0.32 lb/in³
Melting Point (Solidus)1,035°C1,895 °F
Liquidus Temperature1,075°C1,967 °F

Mechanical13

C19100-M11 has a yield strength of 140 MPa (20.3 ksi) and a tensile strength of 310 MPa (45 ksi) — weaker than 74% of copper alloy grades. Elongation at break is 35% and the elastic modulus is 121 GPa (17.5 Msi).

Elastic (Young's) Modulus121 GPa17.5 Msi
Shear Modulus45 GPa6.5 Msi
Bulk Modulus135 GPa19.6 Msi
Poisson's Ratio0.34
Tensile Strength (Ultimate)310 MPa45 ksi
Yield Strength (0.2% offset)140 MPa20.3 ksi
Elongation at Break35%
Reduction in Area45%
Shear Strength275 MPa39.9 ksi
Fatigue Strength (Endurance Limit)165 MPa23.9 ksi
Charpy V-Notch Impact (RT)30 J22.1 ft·lbf
Hardness, Brinell72 HB
Hardness, Rockwell B32 HRB

Thermal6

C19100-M11 is rated for continuous service to 200°C (392 °F). It conducts heat at 150 W/m·K (86.7 BTU/hr·ft·°F), better than 72% of copper alloy grades. Thermal expansion is 17.6 µm/m·K (9.78 µin/in·°F).

Thermal Conductivity150 W/m·K86.7 BTU/hr·ft·°F
Specific Heat Capacity377 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)17.6 µm/m·K9.8 µin/in·°F
Latent Heat of Fusion205 J/g88.1 BTU/lb
Max Service Temperature (continuous)200°C392 °F
Min Service Temperature-196°C-321 °F

Electrical3

C19100-M11 conducts electricity at 35 % IACS, better than 73% of copper alloy grades.

Electrical Conductivity35 % IACS
Electrical Resistivity3.83×10⁻⁸ Ω·m1.51 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (62/100), worse than 57% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.2 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood in fresh/industrial atmospheres, potable water, steam and most non-oxidising acids; attacked by ammonia/amines (SCC risk), oxidising acids, sulphides and mercury compounds.

Sustainability4

Producing a kilogram of C19100-M11 takes about 57 MJ of energy and emits 3.8 kg of CO₂ — less than 52% of copper alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)57 MJ/kg24,506 BTU/lb
Embodied Carbon (primary production)3.8 kg CO₂/kg
Embodied Water220 L/kg26.4 gal/lb
Typical Recycled Content30%

Manufacturability7

C19100-M11's machinability is very good (82/100, better than 90% of copper alloy grades); weldability poor (25/100); formability good (65/100).

MachinabilityVery good82/100
Machinability Rating (AISI 1212 = 100 %)75%
WeldabilityPoor25/100
Formability (cold)Good65/100
Brazeability / SolderabilityVery good70/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper alloy; use tin, nickel or silver plating, or chemical blackening/passivation instead

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

Working with C19100-M11

Is C19100 easy to machine?

Excellent free-cutting behaviour (~80 % of free-cutting brass): use sharp positive-rake carbide or HSS tools, high speed, light feeds and soluble-oil coolant; tellurium gives short chips without lead.

Can C19100 be welded?

Fusion welding is generally avoided — tellurium promotes hot cracking; join by silver brazing, soldering or resistance/friction welding, or use mechanical fastening.

Can C19100 be formed, bent or molded?

Hot forge/extrude at about 750–875 °C then air cool (M10) or quench (M11); cold bending and heading are best done in the quenched or annealed state, followed by 425–500 °C ageing for strength.

What surface finishes work on C19100?

Not anodisable; readily electroplated with Ni, Ag or Sn after cyanide-free acid activation, and takes a bright mechanical polish. Tellurium-bearing turnings should be segregated for recycling.

C19100 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
Niwith Co counted as Ni in some registrations0.6 – 1.20.9
Tefree-machining chip breaker0.35 – 0.70.5
Pforms Ni-P precipitates0.15 – 0.350.25
Pb≤ 0.2—
Zn≤ 0.5—
Fe≤ 0.1—
Cu98.4 % min including Ni, Te, P per CDA registrationbalance—

C19100-M11 — frequently asked

What is C19100-M11 used for?

C19100-M11 is typically used for precision machined electrical parts, connectors and switch components. In short: free-cutting conductive copper; 300 °C service temperature; age-hardenable machining grade.

What is the yield strength of C19100-M11?

C19100-M11 has a typical yield strength of 140 MPa (20.3 ksi) and a tensile strength of 310 MPa (45 ksi) — weaker than 74% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C19100-M11 easy to machine?

Yes — machinability is rated very good (82/100, better than 90% of copper alloy grades). Excellent free-cutting behaviour (~80 % of free-cutting brass): use sharp positive-rake carbide or HSS tools, high speed, light feeds and soluble-oil coolant; tellurium gives short chips without lead.

Can C19100-M11 be welded?

Not readily — weldability is rated poor (25/100). Fusion welding is generally avoided — tellurium promotes hot cracking; join by silver brazing, soldering or resistance/friction welding, or use mechanical fastening.

What surface finishes work on C19100-M11?

Not anodisable; readily electroplated with Ni, Ag or Sn after cyanide-free acid activation, and takes a bright mechanical polish. Tellurium-bearing turnings should be segregated for recycling.

Can C19100-M11 be formed, bent or molded?

Hot forge/extrude at about 750–875 °C then air cool (M10) or quench (M11); cold bending and heading are best done in the quenched or annealed state, followed by 425–500 °C ageing for strength.

What is the maximum service temperature of C19100-M11?

C19100-M11 is rated for continuous use to about 200°C (392 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C19100-TF00 and C19100-OS050?

TF00 is the default condition — pick for maximum strength plus recovered conductivity and best softening resistance in machined electrical parts. OS050: fully soft annealed rod/wire for maximum ductility before heading, upsetting or deep bending. Yield strength is 400 MPa in TF00 versus 105 MPa in OS050.

Sources

  1. Copper Alloy C19100 datasheet (composition, properties, temper table) — Copper Development Association (2024)
  2. ASTM B301 / B441 — Free-Cutting and Tellurium/Nickel-Bearing Copper Rod and Bar — ASTM International (2020)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)

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.