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Copper Alloy C67600-H04

Supply condition

UNS C67600

H04 = full hard

Choose when maximum strength, hardness and wear resistance are needed and little further forming is required.

Premium cost $$$

Values for the H04 condition

Other C67600 tempers and conditions

C67600 is listed in 8 conditions; see the grade overview at C67600.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
As hot extruded
Economical large-section extruded bar/tube for parts that will be fully machined after delivery.20047030110 HB25 % IACS
Soft annealed
Pick for maximum ductility when the part will be further formed, bent or coined before final machining.20545033105 HB25 % IACS
As hot forged and air cooled
Standard condition for hot-forged marine fittings and gear blanks where forged grain flow rather than cold work provides the properties.20548030115 HB25 % IACS
As forged and quenched
Quench from forging heat retains more β phase for higher strength and hardness in heavy wear parts, at some cost in ductility.24052025130 HB24 % IACS
Quarter hard
Light cold draw for straightened rod that still needs moderate bending or upsetting.26051525130 HB24 % IACS
H02Default
Half hard
The standard stocked rod condition: good balance of strength, straightness and machinability for shafts, valve stems and bushings.31056520150 HB24 % IACS
H04This page
Full hard
Choose when maximum strength, hardness and wear resistance are needed and little further forming is required.41562014175 HB24 % IACS
Extra hard
Small-diameter drawn rod/wire where the highest hardness and springiness are wanted; very limited ductility.4706809190 HB23 % IACS

What is C67600-H04?

C67600-H04 is C67600 supplied in the H04 condition — choose when maximum strength, hardness and wear resistance are needed and little further forming is required. C67600-H04 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 620 MPa (89.9 ksi) — stronger than 82% of copper alloy grades. Elongation at break is 14% and the elastic modulus is 103 GPa (14.9 Msi). C67600-H04 has a density of 8.36 g/cm³ (0.302 lb/in³), lighter than 76% of copper alloy grades. It melts at 855°C (1,571 °F). H02 is the default condition FabDigit quotes; H04 is available on request or by drawing note.

Advantages

  • High strength — 415 MPa (60.2 ksi), better than 82% of copper alloy grades
  • Easy to machine — 62/100, better than 75% of copper alloy grades

Limitations

  • Limited service temperature — 150°C (302 °F), worse than 96% of copper alloy grades
  • Difficult to weld — 25/100, worse than 78% of copper alloy grades

C67600-H04 properties

Typical room-temperature values for C67600-H04; 15 are specific to this condition. Other listed values are C67600 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C67600-H04 has a density of 8.36 g/cm³ (0.302 lb/in³), lighter than 76% of copper alloy grades. It melts at 855°C (1,571 °F).

Density8.36 g/cm³0.3 lb/in³
Melting Point (Solidus)855°C1,571 °F
Liquidus Temperature880°C1,616 °F

Mechanical15

C67600-H04 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 620 MPa (89.9 ksi) — stronger than 82% of copper alloy grades. Elongation at break is 14% and the elastic modulus is 103 GPa (14.9 Msi).

Elastic (Young's) Modulus103 GPa14.9 Msi
Shear Modulus39 GPa5.7 Msi
Bulk Modulus115 GPa16.7 Msi
Poisson's Ratio0.34
Tensile Strength (Ultimate)620 MPa89.9 ksi
Yield Strength (0.2% offset)415 MPa60.2 ksi
Elongation at Break14%
Reduction in Area28%
Compressive Strength330 MPa47.9 ksi
Shear Strength370 MPa53.7 ksi
Fatigue Strength (Endurance Limit)195 MPa28.3 ksi
Charpy V-Notch Impact (RT)18 J13.3 ft·lbf
Hardness, Brinell175 HB
Hardness, Rockwell B88 HRB
Hardness, Vickers185 HV

Thermal6

C67600-H04 is rated for continuous service to 150°C (302 °F). It conducts heat at 100 W/m·K (57.8 BTU/hr·ft·°F), better than 54% of copper alloy grades. Thermal expansion is 21.2 µm/m·K (11.8 µin/in·°F).

Thermal Conductivity100 W/m·K57.8 BTU/hr·ft·°F
Specific Heat Capacity377 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)21.2 µm/m·K11.8 µin/in·°F
Latent Heat of Fusion175 J/g75.2 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-200°C-328 °F

Electrical3

C67600-H04 conducts electricity at 24 % IACS, better than 57% of copper alloy grades.

Electrical Conductivity24 % IACS
Electrical Resistivity7.2×10⁻⁸ Ω·m2.83 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (55/100), worse than 86% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.28 V
Corrosion ResistanceGood55/100
Chemical Resistance SummaryGood in seawater, brine and neutral waters; susceptible to dezincification in stagnant/acidic chloride water and to stress-corrosion cracking in ammonia; avoid oxidizing acids, ferric/mercury salts and hydrogen sulfide.

Sustainability4

Producing a kilogram of C67600-H04 takes about 57 MJ of energy and emits 3.7 kg of CO₂ — less than 52% of copper alloy grades. Typical recycled content is 55%.

Embodied Energy (primary production)57 MJ/kg24,506 BTU/lb
Embodied Carbon (primary production)3.7 kg CO₂/kg
Embodied Water320 L/kg38.3 gal/lb
Typical Recycled Content55%

Manufacturability8

C67600-H04's machinability is good (62/100, better than 75% of copper alloy grades); weldability poor (25/100); formability poor (20/100).

MachinabilityGood62/100
Machinability Rating (AISI 1212 = 100 %)55%
WeldabilityPoor25/100
Formability (cold)Poor20/100
CastabilityGood65/100
Brazeability / SolderabilityGood60/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper alloy; use chromate/benzotriazole passivation, tin or nickel plating instead

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

Working with C67600-H04

Is C67600 easy to machine?

Free-machining for a high-strength brass thanks to the lead: use sharp carbide, 0° to slightly positive rake, high speed and light feed; chips break well but the β phase is abrasive, so expect more tool wear than C36000.

Can C67600 be welded?

Fusion welding is not recommended (lead cracking, zinc fume); join by silver brazing, soft soldering or mechanical fastening with adequate ventilation.

Can C67600 be formed, bent or molded?

Excellent hot workability at 650–760 °C (hot forging/extrusion is the preferred route); cold formability is limited — anneal at ~500–600 °C between severe operations.

What surface finishes work on C67600?

Takes a bright mechanical polish; anodizing is not applicable — protect with benzotriazole passivation, lacquer, tin or nickel plating, and avoid ammonia-based cleaners to prevent SCC.

C67600 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
Cu57 – 6058.5
Sn0.5 – 1.51
Fe0.4 – 1.30.8
MnChinese HMn58-2 practice runs Mn 1.0–2.0 %0.05 – 0.50.3
Pbadded for machinability0.3 – 10.6
Al≤ 0.250.1
Znremainder, approx. 37–40 %balance—

C67600-H04 — frequently asked

What is C67600-H04 used for?

C67600-H04 is typically used for ship propeller hubs, valve stems, gears and bushings and marine hardware requiring machining. In short: machinable high-strength bronze; forged marine load hardware; not fusion weldable.

What is the yield strength of C67600-H04?

C67600-H04 has a typical yield strength of 415 MPa (60.2 ksi) and a tensile strength of 620 MPa (89.9 ksi) — stronger than 82% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C67600-H04 easy to machine?

Reasonably — machinability is rated good (62/100, better than 75% of copper alloy grades). Free-machining for a high-strength brass thanks to the lead: use sharp carbide, 0° to slightly positive rake, high speed and light feed; chips break well but the β phase is abrasive, so expect more tool wear than C36000.

Can C67600-H04 be welded?

Not readily — weldability is rated poor (25/100). Fusion welding is not recommended (lead cracking, zinc fume); join by silver brazing, soft soldering or mechanical fastening with adequate ventilation.

What surface finishes work on C67600-H04?

Takes a bright mechanical polish; anodizing is not applicable — protect with benzotriazole passivation, lacquer, tin or nickel plating, and avoid ammonia-based cleaners to prevent SCC.

Can C67600-H04 be formed, bent or molded?

Excellent hot workability at 650–760 °C (hot forging/extrusion is the preferred route); cold formability is limited — anneal at ~500–600 °C between severe operations.

What is the maximum service temperature of C67600-H04?

C67600-H04 is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C67600-H02 and C67600-H06?

H02 is the default condition — the standard stocked rod condition: good balance of strength, straightness and machinability for shafts, valve stems and bushings. H06: small-diameter drawn rod/wire where the highest hardness and springiness are wanted; very limited ductility. Yield strength is 310 MPa in H02 versus 470 MPa in H06.

Sources

  1. ASTM B138/B138M — Manganese Bronze Rod, Bar and Shapes — ASTM International (2019)
  2. CDA / UNS Standard Designations for Wrought Copper Alloys (C676xx manganese bronze) — Copper Development Association (2023)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  4. GB/T 4423 / GB/T 5232 (HMn58-2 ) (2020)

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.