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Copper Alloy C15900-H08

Supply condition

UNS C15900

H08 = spring hard

Highest strength condition, used for fine wire, contact springs and small-diameter conductors.

High cost $$$$

Values for the H08 condition

Other C15900 tempers and conditions

C15900 is listed in 7 conditions; see the grade overview at C15900.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Hot isostatic pressed
Consolidated powder billet supplied for customers who will forge, extrude or back-extrude the part themselves.31040022105 HB86 % IACS
As hot extruded
Pick for large-section bar, forging stock and parts that will be heavily machined or subsequently hot worked.37045020118 HB86 % IACS
Cold worked then stress relieved / brazing-cycle exposed
Represents the property level after vacuum brazing or high-temperature stress relief — chosen when the part must be joined or thermally cycled and still carry load.39547018125 HB86 % IACS
Quarter hard
Compromise temper when some bending/staking is still required but higher yield than mill condition is wanted.43049016130 HB85 % IACS
Half hard
Typical for strip, small rod and contact supports needing balanced strength and residual ductility.47051514138 HB85 % IACS
H04Default
Full hard
Standard stocked condition for resistance-welding electrodes, high heat-flux inserts and structural conductors.50555012145 HB85 % IACS
H08This page
Spring hard
Highest strength condition, used for fine wire, contact springs and small-diameter conductors.5706108160 HB84 % IACS

What is C15900-H08?

C15900-H08 is C15900 supplied in the H08 condition — highest strength condition, used for fine wire, contact springs and small-diameter conductors. C15900-H08 has a yield strength of 570 MPa (82.7 ksi) and a tensile strength of 610 MPa (88.5 ksi) — stronger than 93% of copper alloy grades. Elongation at break is 8% and the elastic modulus is 130 GPa (18.9 Msi). C15900-H08 has a density of 8.86 g/cm³ (0.32 lb/in³), heavier than 68% of copper alloy grades. It melts at 1,083°C (1,981 °F). H04 is the default condition FabDigit quotes; H08 is available on request or by drawing note.

Advantages

  • High service temperature — 450°C (842 °F), better than 98% of copper alloy grades
  • High strength — 570 MPa (82.7 ksi), better than 93% of copper alloy grades
  • Stiff — 130 GPa (18.9 Msi), better than 89% of copper alloy grades
  • Conducts heat well — 325 W/m·K (187.8 BTU/hr·ft·°F), better than 85% of copper alloy grades
  • High electrical conductivity — 84 % IACS, better than 85% of copper alloy grades

Limitations

  • Difficult to weld — 20/100, worse than 88% of copper alloy grades
  • Hard to polish — 65/100, worse than 87% of copper alloy grades
  • Limited ductility — 8%, worse than 83% of copper alloy grades

C15900-H08 properties

Typical room-temperature values for C15900-H08; 22 are specific to this condition. Other listed values are C15900 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C15900-H08 has a density of 8.86 g/cm³ (0.32 lb/in³), heavier than 68% of copper alloy grades. It melts at 1,083°C (1,981 °F).

Density8.86 g/cm³0.32 lb/in³
Melting Point (Solidus)1,083°C1,981 °F
Liquidus Temperature1,083°C1,981 °F

Mechanical13

C15900-H08 has a yield strength of 570 MPa (82.7 ksi) and a tensile strength of 610 MPa (88.5 ksi) — stronger than 93% of copper alloy grades. Elongation at break is 8% and the elastic modulus is 130 GPa (18.9 Msi).

Elastic (Young's) Modulus130 GPa18.9 Msi
Shear Modulus48 GPa7 Msi
Bulk Modulus140 GPa20.3 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)610 MPa88.5 ksi
Yield Strength (0.2% offset)570 MPa82.7 ksi
Elongation at Break8%
Reduction in Area55%
Shear Strength355 MPa51.5 ksi
Fatigue Strength (Endurance Limit)230 MPa33.4 ksi
Hardness, Brinell160 HB
Hardness, Rockwell B84 HRB
Hardness, Vickers168 HV

Thermal6

C15900-H08 is rated for continuous service to 450°C (842 °F). It conducts heat at 325 W/m·K (187.8 BTU/hr·ft·°F), better than 85% of copper alloy grades. Thermal expansion is 16.6 µm/m·K (9.22 µin/in·°F).

Thermal Conductivity325 W/m·K188 BTU/hr·ft·°F
Specific Heat Capacity380 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.6 µm/m·K9.2 µin/in·°F
Latent Heat of Fusion205 J/g88.1 BTU/lb
Max Service Temperature (continuous)450°C842 °F
Min Service Temperature-269°C-452 °F

Electrical3

C15900-H08 conducts electricity at 84 % IACS, better than 85% of copper alloy grades.

Electrical Conductivity84 % IACS
Electrical Resistivity2.05×10⁻⁸ Ω·m0.807 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)-0.22 V
Corrosion ResistanceGood55/100
Chemical Resistance SummaryBehaves essentially like pure copper: good in fresh/sea water, neutral salts and non-oxidising acids; attacked by ammonia/amines, oxidising acids (HNO₃), sulphides and moist halogens. Al₂O₃ dispersoid gives a slight benefit against high-temperature scaling but does not change aqueous behaviour.

Sustainability4

Producing a kilogram of C15900-H08 takes about 65 MJ of energy and emits 4.2 kg of CO₂ — more than 81% of copper alloy grades. Typical recycled content is 5%.

Embodied Energy (primary production)65 MJ/kg27,945 BTU/lb
Embodied Carbon (primary production)4.2 kg CO₂/kg
Embodied Water320 L/kg38.3 gal/lb
Typical Recycled Content5%

Manufacturability7

C15900-H08's machinability is poor (30/100, worse than 67% of copper alloy grades); weldability poor (20/100); formability poor (20/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)18%
WeldabilityPoor20/100
Formability (cold)Poor20/100
Brazeability / SolderabilityExcellent85/100
PolishabilityGood65/100
Anodizing Responsen/a — copper alloy, not anodised; use electroplating (Ni, Ag, Cr) or bare oxide-resistant service

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

Working with C15900-H08

Is C15900 easy to machine?

Machines like tough copper but the Al₂O₃ is abrasive — use sharp, polished uncoated carbide or PCD, positive rake, high speed with flood coolant, and expect 3–5× the tool wear of C11000.

Can C15900 be welded?

Avoid fusion welding (GTAW/GMAW) — melting agglomerates the dispersoid and causes porosity; join by vacuum/furnace brazing, electron-beam, friction or resistance welding, all of which leave the base metal strength intact.

Can C15900 be formed, bent or molded?

Cold form only with generous radii and limited reduction per pass; hot working (700–900 °C extrusion/forging) is the normal route and does not soften the material.

What surface finishes work on C15900?

Not anodisable; electroplate Ni, Ag or hard Cr for wear/oxidation protection, or leave bare with periodic oxide removal — polishes to a copper lustre but the dispersoid can leave a slightly matte finish.

C15900 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
Alpresent as internally-oxidised Al₂O₃ dispersoid (≈0.4–1.1 wt% Al₂O₃), not in solid solution0.2 – 0.60.35
Ocombined as Al₂O₃; residual free oxygen kept low0.15 – 0.550.3
Other (each)incidental impurities from powder route≤ 0.05—
Cumatrix, high-purity oxygen-free copperbalance—

C15900-H08 — frequently asked

What is C15900-H08 used for?

C15900-H08 is typically used for resistance welding electrodes, rocket engine combustion chamber liners and high-temperature electrical contacts. In short: highest-temperature conductive copper; non-softening to 500 °C; dispersion-strengthened, not age-hardened.

What is the yield strength of C15900-H08?

C15900-H08 has a typical yield strength of 570 MPa (82.7 ksi) and a tensile strength of 610 MPa (88.5 ksi) — stronger than 93% of copper alloy grades. Strength varies by condition: see the 7 listed tempers.

Is C15900-H08 easy to machine?

Not especially — machinability is rated poor (30/100, worse than 67% of copper alloy grades). Machines like tough copper but the Al₂O₃ is abrasive — use sharp, polished uncoated carbide or PCD, positive rake, high speed with flood coolant, and expect 3–5× the tool wear of C11000.

Can C15900-H08 be welded?

Not readily — weldability is rated poor (20/100). Avoid fusion welding (GTAW/GMAW) — melting agglomerates the dispersoid and causes porosity; join by vacuum/furnace brazing, electron-beam, friction or resistance welding, all of which leave the base metal strength intact.

What surface finishes work on C15900-H08?

Not anodisable; electroplate Ni, Ag or hard Cr for wear/oxidation protection, or leave bare with periodic oxide removal — polishes to a copper lustre but the dispersoid can leave a slightly matte finish.

Can C15900-H08 be formed, bent or molded?

Cold form only with generous radii and limited reduction per pass; hot working (700–900 °C extrusion/forging) is the normal route and does not soften the material.

What is the maximum service temperature of C15900-H08?

C15900-H08 is rated for continuous use to about 450°C (842 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C15900-H04 and C15900-HIP?

H04 is the default condition — standard stocked condition for resistance-welding electrodes, high heat-flux inserts and structural conductors. HIP: consolidated powder billet supplied for customers who will forge, extrude or back-extrude the part themselves. Yield strength is 505 MPa in H04 versus 310 MPa in HIP.

Sources

  1. ASTM B902 — Compacted and Sintered Dispersion-Strengthened Copper Structural Materials — ASTM International (2020)
  2. CDA/UNS Copper Alloy Registration — C159xx dispersion-strengthened coppers — Copper Development Association (2023)
  3. GlidCop Dispersion Strengthened Copper AL-15 / AL-25 / AL-60 property data — SCM Metal Products / Höganäs (2019)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose Materials — 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.