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Copper Alloy C46200-H04

Supply condition

UNS C46200 · ASTM B21

H04 = full hard

Highest-strength wrought temper for small-diameter rod, wire and screw-machine stock where bending is not required.

High cost $$$$

Values for the H04 condition

Other C46200 tempers and conditions

C46200 is listed in 6 conditions; see the grade overview at C46200.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Pick for maximum ductility before severe bending, spinning or deep forming of naval brass sections.1703854795 HB—
M30Default
As hot extruded
Standard stock condition for naval brass rod, bar and shapes; best all-round strength-to-ductility for machined marine hardware.18040040100 HB26 % IACS
Light annealed
Partially softened condition giving a compromise between formability and dimensional stability of drawn rod and tube.20541538112 HB—
Cold formed
Light cold-work temper used for cold-headed fasteners and formed parts where some residual ductility must remain.27545027135 HB—
Half hard
Cold-drawn rod temper for shafts, valve stems and marine fasteners needing higher yield strength with usable ductility.36047020150 HB—
H04This page
Full hard
Highest-strength wrought temper for small-diameter rod, wire and screw-machine stock where bending is not required.41556015180 HB—

What is C46200-H04?

C46200-H04 is C46200 supplied in the H04 condition — highest-strength wrought temper for small-diameter rod, wire and screw-machine stock where bending is not required. C46200-H04 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 560 MPa (81.2 ksi) — stronger than 82% of copper alloy grades. Elongation at break is 15% and the elastic modulus is 100 GPa (14.5 Msi). C46200-H04 has a density of 8.41 g/cm³ (0.304 lb/in³), lighter than 72% of copper alloy grades. It melts at 885°C (1,625 °F). M30 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

Limitations

  • Limited service temperature — 150°C (302 °F), worse than 96% of copper alloy grades
  • Low stiffness — 100 GPa (14.5 Msi), worse than 82% of copper alloy grades
  • Limited formability — 18/100, worse than 75% of copper alloy grades

C46200-H04 properties

Typical room-temperature values for C46200-H04; 13 are specific to this condition. Other listed values are C46200 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C46200-H04 has a density of 8.41 g/cm³ (0.304 lb/in³), lighter than 72% of copper alloy grades. It melts at 885°C (1,625 °F).

Density8.41 g/cm³0.3 lb/in³
Melting Point (Solidus)885°C1,625 °F
Liquidus Temperature900°C1,652 °F

Mechanical13

C46200-H04 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 560 MPa (81.2 ksi) — stronger than 82% of copper alloy grades. Elongation at break is 15% and the elastic modulus is 100 GPa (14.5 Msi).

Elastic (Young's) Modulus100 GPa14.5 Msi
Shear Modulus38 GPa5.5 Msi
Bulk Modulus110 GPa16 Msi
Poisson's Ratio0.34
Tensile Strength (Ultimate)560 MPa81.2 ksi
Yield Strength (0.2% offset)415 MPa60.2 ksi
Elongation at Break15%
Reduction in Area32%
Shear Strength315 MPa45.7 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Hardness, Brinell180 HB
Hardness, Rockwell B90 HRB
Hardness, Vickers190 HV

Thermal6

C46200-H04 is rated for continuous service to 150°C (302 °F). It conducts heat at 116 W/m·K (67 BTU/hr·ft·°F), better than 64% of copper alloy grades. Thermal expansion is 21.2 µm/m·K (11.8 µin/in·°F).

Thermal Conductivity116 W/m·K67 BTU/hr·ft·°F
Specific Heat Capacity380 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 Fusion170 J/g73.1 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-200°C-328 °F

Electrical3

C46200-H04 conducts electricity at 26 % IACS, better than 63% of copper alloy grades.

Electrical Conductivity26 % IACS
Electrical Resistivity6.6×10⁻⁸ Ω·m2.6 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)-0.3 V
Corrosion ResistanceGood55/100
Chemical Resistance SummaryGood in seawater, brackish water and neutral salts; resists atmospheric and steam corrosion. Susceptible to dezincification (no arsenic inhibitor) in stagnant/hot chloride water, and to stress-corrosion cracking in ammonia, amines and mercury salts; attacked by oxidizing acids, ferric/chromic solutions and hydrogen sulphide.

Sustainability4

Producing a kilogram of C46200-H04 takes about 57 MJ of energy and emits 3.9 kg of CO₂ — less than 52% of copper alloy grades. Typical recycled content is 45%.

Embodied Energy (primary production)57 MJ/kg24,506 BTU/lb
Embodied Carbon (primary production)3.9 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content45%

Manufacturability8

C46200-H04's machinability is fair (52/100, better than 69% of copper alloy grades); weldability fair (45/100); formability poor (18/100).

MachinabilityFair52/100
Machinability Rating (AISI 1212 = 100 %)95%
WeldabilityFair45/100
Formability (cold)Poor18/100
CastabilityGood55/100
Brazeability / SolderabilityExcellent90/100
PolishabilityVery good80/100
Anodizing Responsen/a — copper alloy; use chromate/benzotriazole passivation, tin or nickel plating, or clear lacquer instead

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

Working with C46200-H04

Is C46200 easy to machine?

Machines readily with sharp positive-rake tooling at ~30% of free-cutting brass rate; chips are stringier than C36000 because Pb is limited, so use chipbreakers and generous coolant.

Can C46200 be welded?

Best joined by brazing or soldering; GTAW/oxyfuel with silicon-bronze or naval-brass filler is possible but zinc fuming, porosity and colour mismatch require good ventilation and low heat input.

Can C46200 be formed, bent or molded?

Excellent hot forgeability/extrudability at 650–760 °C; cold formability only fair due to the beta phase — anneal at 425–600 °C between severe forming steps.

What surface finishes work on C46200?

Takes a bright mechanical or buffed polish; not anodizable — protect with benzotriazole/chromate passivation, clear lacquer, or nickel/tin/chrome plating; stress-relieve cold-worked parts at ~275 °C to avoid season cracking.

C46200 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
Cu62 – 6563.5
Sn0.5 – 10.7
Pb≤ 0.20.05
Fe≤ 0.10.05
Znbalance—

C46200-H04 — frequently asked

What is C46200-H04 used for?

C46200-H04 is typically used for marine hardware, propeller shafts and fittings, valve stems and condenser plates. In short: naval brass without inhibitor; forgeable marine rod grade; mid-strength seawater alloy.

What is the yield strength of C46200-H04?

C46200-H04 has a typical yield strength of 415 MPa (60.2 ksi) and a tensile strength of 560 MPa (81.2 ksi) — stronger than 82% of copper alloy grades. Strength varies by condition: see the 6 listed tempers.

Is C46200-H04 easy to machine?

Reasonably — machinability is rated fair (52/100, better than 69% of copper alloy grades). Machines readily with sharp positive-rake tooling at ~30% of free-cutting brass rate; chips are stringier than C36000 because Pb is limited, so use chipbreakers and generous coolant.

Can C46200-H04 be welded?

With care — weldability is rated fair (45/100). Best joined by brazing or soldering; GTAW/oxyfuel with silicon-bronze or naval-brass filler is possible but zinc fuming, porosity and colour mismatch require good ventilation and low heat input.

What surface finishes work on C46200-H04?

Takes a bright mechanical or buffed polish; not anodizable — protect with benzotriazole/chromate passivation, clear lacquer, or nickel/tin/chrome plating; stress-relieve cold-worked parts at ~275 °C to avoid season cracking.

Can C46200-H04 be formed, bent or molded?

Excellent hot forgeability/extrudability at 650–760 °C; cold formability only fair due to the beta phase — anneal at 425–600 °C between severe forming steps.

What is the maximum service temperature of C46200-H04?

C46200-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 C46200-M30 and C46200-H04?

M30 is the default condition — standard stock condition for naval brass rod, bar and shapes; best all-round strength-to-ductility for machined marine hardware. H04: highest-strength wrought temper for small-diameter rod, wire and screw-machine stock where bending is not required. Yield strength is 180 MPa in M30 versus 415 MPa in H04.

Sources

  1. ASTM B21/B21M — Naval Brass Rod, Bar and Shapes — ASTM International (2021)
  2. ASTM B124 — Copper and Copper-Alloy Forging Rod, Bar and Shapes — ASTM International (2020)
  3. CDA Alloy Database — C46200 / C46400 Naval Brass — Copper Development Association (copper.org) (2023)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. ASM Handbook Vol. 13B — Corrosion: Materials (copper alloys in seawater) — ASM International (2005)

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.