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Copper Alloy C48200-H50

Supply condition

UNS C48200 · ASTM B21 · EN CW714R · JIS C4802

H50 = extruded and drawn

Choose when close diameter tolerance and a straight, bright bar are needed with only moderate strengthening.

High cost $$$$

Values for the H50 condition

Other C48200 tempers and conditions

C48200 is listed in 8 conditions; see the grade overview at C48200.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Fully recrystallised, lowest strength and highest ductility; choose for maximum cold forming, flaring or spinning and to eliminate residual-stress cracking.1503724585 HB—
M30Default
As hot extruded
Standard stock condition for round/hex bar and shapes; best ductility with good machinability, pick for general turned parts and further forging.17237940100 HB26 % IACS
As hot forged and air cooled
Standard delivery state for hot-forged marine hardware and valve bodies; sound wrought structure with good ductility, no post-forge treatment.18641433105 HB26 % IACS
Light annealed
Partial anneal that relieves drawing stresses (SCC risk) while keeping some strength; a good compromise before moderate bending or staking.1904004095 HB26 % IACS
As forged and quenched
Water-quenched straight off the press to retain a finer β structure; slightly stronger and harder forgings with less scale, used where dimensional and strength consistency matter.20544830115 HB25 % IACS
H50This page
Extruded and drawn
Choose when close diameter tolerance and a straight, bright bar are needed with only moderate strengthening.27544825125 HB—
Half hard
Best balance of strength, straightness and chip control for valve stems, screw-machine parts and threaded fittings.34548320140 HB—
Full hard
Highest strength and stiffness in service; use for wear surfaces, small-diameter stems and springs where ductility is not required.40051715160 HB—

What is C48200-H50?

C48200-H50 is C48200 supplied in the H50 condition — choose when close diameter tolerance and a straight, bright bar are needed with only moderate strengthening. C48200-H50 has a yield strength of 275 MPa (39.9 ksi) and a tensile strength of 448 MPa (65 ksi) — stronger than 57% of copper alloy grades. Elongation at break is 25% and the elastic modulus is 100 GPa (14.5 Msi). C48200-H50 has a density of 8.44 g/cm³ (0.305 lb/in³), lighter than 70% of copper alloy grades. It melts at 885°C (1,625 °F). M30 is the default condition FabDigit quotes; H50 is available on request or by drawing note.

Advantages

  • Low embodied carbon — 3.2 kg CO₂/kg, better than 92% of copper alloy grades
  • Easy to machine — 72/100, better than 79% of copper alloy grades

Limitations

  • Low stiffness — 100 GPa (14.5 Msi), worse than 82% of copper alloy grades
  • Difficult to weld — 25/100, worse than 78% of copper alloy grades

C48200-H50 properties

Typical room-temperature values for C48200-H50; 11 are specific to this condition. Other listed values are C48200 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C48200-H50 has a density of 8.44 g/cm³ (0.305 lb/in³), lighter than 70% of copper alloy grades. It melts at 885°C (1,625 °F).

Density8.44 g/cm³0.3 lb/in³
Melting Point (Solidus)885°C1,625 °F
Liquidus Temperature900°C1,652 °F

Mechanical14

C48200-H50 has a yield strength of 275 MPa (39.9 ksi) and a tensile strength of 448 MPa (65 ksi) — stronger than 57% of copper alloy grades. Elongation at break is 25% and the elastic modulus is 100 GPa (14.5 Msi).

Elastic (Young's) Modulus100 GPa14.5 Msi
Shear Modulus37 GPa5.4 Msi
Bulk Modulus110 GPa16 Msi
Poisson's Ratio0.34
Tensile Strength (Ultimate)448 MPa65 ksi
Yield Strength (0.2% offset)275 MPa39.9 ksi
Elongation at Break25%
Reduction in Area40%
Shear Strength295 MPa42.8 ksi
Fatigue Strength (Endurance Limit)145 MPa21 ksi
Charpy V-Notch Impact (RT)30 J22.1 ft·lbf
Hardness, Brinell125 HB
Hardness, Rockwell B70 HRB
Hardness, Vickers105 HV

Thermal6

C48200-H50 is rated for continuous service to 200°C (392 °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 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 Fusion170 J/g73.1 BTU/lb
Max Service Temperature (continuous)200°C392 °F
Min Service Temperature-200°C-328 °F

Electrical3

C48200-H50 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 (62/100), worse than 57% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.3 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood in seawater, brines and neutral waters; tin addition limits dezincification but the alloy is not fully inhibited (no As). Attacked by ammonia/amines (stress-corrosion cracking), oxidising acids, mercury salts, acetylene and high-velocity aerated seawater above ~2 m/s.

Sustainability4

Producing a kilogram of C48200-H50 takes about 53 MJ of energy and emits 3.2 kg of CO₂ — less than 85% of copper alloy grades. Typical recycled content is 60%.

Embodied Energy (primary production)53 MJ/kg22,786 BTU/lb
Embodied Carbon (primary production)3.2 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content60%

Manufacturability8

C48200-H50's machinability is very good (72/100, better than 79% of copper alloy grades); weldability poor (25/100); formability fair (35/100).

MachinabilityVery good72/100
Machinability Rating (AISI 1212 = 100 %)72%
WeldabilityPoor25/100
Formability (cold)Fair35/100
CastabilityFair45/100
Brazeability / SolderabilityExcellent85/100
PolishabilityVery good80/100
Anodizing Responsen/a — copper alloy; use chromate/benzotriazole passivation, lacquer, nickel or chrome plating instead

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

Working with C48200-H50

Is C48200 easy to machine?

Excellent free-cutting behaviour (~70% of AISI 1212); use zero-to-negative rake brass geometry, high speed, light lubricant — chips break short thanks to the lead.

Can C48200 be welded?

Arc/resistance welding not recommended (lead hot-cracking and zinc fume); join by soldering, brazing or mechanical means with good ventilation.

Can C48200 be formed, bent or molded?

Hot working (650–780 °C) and hot forging are excellent; cold formability is only fair — anneal or use O60 before severe bending, and stress-relieve to avoid ammonia SCC.

What surface finishes work on C48200?

Takes a high mechanical or electro-polish; commonly chrome/nickel plated or lacquered; not anodizable — benzotriazole or chromate passivation for tarnish control.

C48200 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
Cu59 – 6260.5
Sninhibits dezincification0.5 – 10.75
Pbfree-machining addition0.4 – 10.7
Fe≤ 0.10.03
Znbalance—

C48200-H50 — frequently asked

What is C48200-H50 used for?

C48200-H50 is typically used for valve stems, marine fittings and machined marine hardware. In short: best-machining naval brass; free-cutting marine rod; screw-machine marine parts.

What is the yield strength of C48200-H50?

C48200-H50 has a typical yield strength of 275 MPa (39.9 ksi) and a tensile strength of 448 MPa (65 ksi) — stronger than 57% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C48200-H50 easy to machine?

Yes — machinability is rated very good (72/100, better than 79% of copper alloy grades). Excellent free-cutting behaviour (~70% of AISI 1212); use zero-to-negative rake brass geometry, high speed, light lubricant — chips break short thanks to the lead.

Can C48200-H50 be welded?

Not readily — weldability is rated poor (25/100). Arc/resistance welding not recommended (lead hot-cracking and zinc fume); join by soldering, brazing or mechanical means with good ventilation.

What surface finishes work on C48200-H50?

Takes a high mechanical or electro-polish; commonly chrome/nickel plated or lacquered; not anodizable — benzotriazole or chromate passivation for tarnish control.

Can C48200-H50 be formed, bent or molded?

Hot working (650–780 °C) and hot forging are excellent; cold formability is only fair — anneal or use O60 before severe bending, and stress-relieve to avoid ammonia SCC.

What is the maximum service temperature of C48200-H50?

C48200-H50 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 C48200-M30 and C48200-H04?

M30 is the default condition — standard stock condition for round/hex bar and shapes; best ductility with good machinability, pick for general turned parts and further forging. H04: highest strength and stiffness in service; use for wear surfaces, small-diameter stems and springs where ductility is not required. Yield strength is 172 MPa in M30 versus 400 MPa in H04.

Sources

  1. CDA Alloy Datasheet C48200 (leaded naval brass) — Copper Development Association (2023)
  2. ASTM B21/B21M — Naval Brass Rod, Bar and Shapes — ASTM International (2021)
  3. ASTM B283/B283M — Copper and Copper-Alloy Die Forgings — ASTM International (2020)
  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.