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Copper Alloy C74500-H08

Supply condition

UNS C74500

H08 = spring hard

Spring-temper strip for contact springs, diaphragms and snap parts; bend only with generous radii and grain-direction control.

High cost $$$$

Values for the H08 condition

Other C74500 tempers and conditions

C74500 is listed in 8 conditions; see the grade overview at C74500.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Pick for deep drawing, severe bending and spinning where maximum ductility is needed.1553854095 HB9 % IACS
As hot rolled
Hot-rolled plate/bar stock for machined or further-worked parts where temper control is not critical.17040035100 HB—
Quarter hard
Choose when moderate strength must be combined with substantial bending/forming ability.34045020130 HB—
H02Default
Half hard
The general-purpose stocked strip temper: good balance of strength, flatness and forming for hardware and decorative parts.40051012150 HB—
Full hard
Use for stamped flat parts and light spring contacts needing high strength with only gentle bends.5155854175 HB—
Extra hard
For flat springs, clips and blanked parts where stiffness and yield strength dominate over formability.5906503190 HB—
H08This page
Spring hard
Spring-temper strip for contact springs, diaphragms and snap parts; bend only with generous radii and grain-direction control.6356902200 HB—
Extra spring hard
Maximum-strength cold-rolled strip for highly stressed flat springs; essentially no formability.675725217 HRC8.5 % IACS

What is C74500-H08?

C74500-H08 is C74500 supplied in the H08 condition — spring-temper strip for contact springs, diaphragms and snap parts; bend only with generous radii and grain-direction control. C74500-H08 has a yield strength of 635 MPa (92.1 ksi) and a tensile strength of 690 MPa (100 ksi) — stronger than 95% of copper alloy grades. Elongation at break is 2% and the elastic modulus is 127 GPa (18.4 Msi). C74500-H08 has a density of 8.73 g/cm³ (0.315 lb/in³), lighter than 53% of copper alloy grades. It melts at 954°C (1,749 °F). H02 is the default condition FabDigit quotes; H08 is available on request or by drawing note.

Advantages

  • Polishes to a fine finish — 90/100, better than 99% of copper alloy grades
  • High strength — 635 MPa (92.1 ksi), better than 95% of copper alloy grades

Limitations

  • Limited service temperature — 140°C (284 °F), worse than 100% of copper alloy grades
  • Limited ductility — 2%, worse than 98% of copper alloy grades
  • High embodied carbon — 5.2 kg CO₂/kg, worse than 88% of copper alloy grades
  • Low electrical conductivity — 9 % IACS, worse than 78% of copper alloy grades
  • Poor heat conductor — 45 W/m·K (26 BTU/hr·ft·°F), worse than 76% of copper alloy grades

C74500-H08 properties

Typical room-temperature values for C74500-H08; 12 are specific to this condition. Other listed values are C74500 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C74500-H08 has a density of 8.73 g/cm³ (0.315 lb/in³), lighter than 53% of copper alloy grades. It melts at 954°C (1,749 °F).

Density8.73 g/cm³0.32 lb/in³
Melting Point (Solidus)954°C1,749 °F
Liquidus Temperature1,021°C1,870 °F

Mechanical12

C74500-H08 has a yield strength of 635 MPa (92.1 ksi) and a tensile strength of 690 MPa (100 ksi) — stronger than 95% of copper alloy grades. Elongation at break is 2% and the elastic modulus is 127 GPa (18.4 Msi).

Elastic (Young's) Modulus127 GPa18.4 Msi
Shear Modulus48 GPa7 Msi
Bulk Modulus128 GPa18.6 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)690 MPa100 ksi
Yield Strength (0.2% offset)635 MPa92.1 ksi
Elongation at Break2%
Shear Strength395 MPa57.3 ksi
Fatigue Strength (Endurance Limit)215 MPa31.2 ksi
Hardness, Brinell200 HB
Hardness, Rockwell B93 HRB
Hardness, Vickers212 HV

Thermal6

C74500-H08 is rated for continuous service to 140°C (284 °F). It conducts heat at 45 W/m·K (26 BTU/hr·ft·°F), worse than 76% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity45 W/m·K26 BTU/hr·ft·°F
Specific Heat Capacity377 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.2 µm/m·K9 µin/in·°F
Latent Heat of Fusion195 J/g83.8 BTU/lb
Max Service Temperature (continuous)140°C284 °F
Min Service Temperature-200°C-328 °F

Electrical3

C74500-H08 conducts electricity at 9 % IACS, worse than 78% of copper alloy grades.

Electrical Conductivity9 % IACS
Electrical Resistivity1.92×10⁻⁷ Ω·m7.56 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)-0.26 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood resistance to atmosphere, fresh water and mild organic media; better tarnish resistance than brass. Attacked by ammonia/amines (SCC risk in cold-worked tempers), oxidising acids, sulphides and rapid seawater flow.

Sustainability4

Producing a kilogram of C74500-H08 takes about 78 MJ of energy and emits 5.2 kg of CO₂ — more than 90% of copper alloy grades. Typical recycled content is 40%.

Embodied Energy (primary production)78 MJ/kg33,534 BTU/lb
Embodied Carbon (primary production)5.2 kg CO₂/kg
Embodied Water260 L/kg31.2 gal/lb
Typical Recycled Content40%

Manufacturability7

C74500-H08's machinability is poor (33/100, worse than 53% of copper alloy grades); weldability fair (40/100); formability poor (18/100).

MachinabilityPoor33/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityFair40/100
Formability (cold)Poor18/100
Brazeability / SolderabilityExcellent88/100
PolishabilityExcellent90/100
Anodizing Responsen/a — copper alloy; use bright polish, lacquer, nickel/chrome or silver plating instead

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

Working with C74500-H08

Is C74500 easy to machine?

Machinability only ~20% of free-cutting brass — gummy, long chips; use sharp positive-rake tools, high speed, low feed and generous lubrication; leaded nickel silvers (C79300) are preferable for screw-machine work.

Can C74500 be welded?

Arc/gas fusion welding is poor because zinc fumes and volatilises; resistance spot/seam welding is good and silver brazing or soldering is excellent — use ventilation and low-zinc filler when fusion joining is unavoidable.

Can C74500 be formed, bent or molded?

Excellent cold formability in O61/H01 (deep drawing, spinning, coining); interanneal ~600–700 °C, and stress-relieve cold-worked parts at ~250–300 °C to avoid ammonia-related stress-corrosion cracking.

What surface finishes work on C74500?

Takes a bright white mirror polish directly and is a standard base for nickel, chrome, silver or gold plating; lacquer or clear coat outdoors to prevent slow tarnish — cannot be anodized.

C74500 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
CuCu incl. Ag63.5 – 66.565
NiNi + Co9 – 1110
Pb≤ 0.1—
Fe≤ 0.25—
Mn≤ 0.5—
Znremainder, ~25%balance—

C74500-H08 — frequently asked

What is C74500-H08 used for?

C74500-H08 is typically used for zippers, eyeglass frames, hardware, electrical connectors and nameplates. In short: classic 65-10 nickel silver; bright white plating base; not for screw machining.

What is the yield strength of C74500-H08?

C74500-H08 has a typical yield strength of 635 MPa (92.1 ksi) and a tensile strength of 690 MPa (100 ksi) — stronger than 95% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C74500-H08 easy to machine?

Not especially — machinability is rated poor (33/100, worse than 53% of copper alloy grades). Machinability only ~20% of free-cutting brass — gummy, long chips; use sharp positive-rake tools, high speed, low feed and generous lubrication; leaded nickel silvers (C79300) are preferable for screw-machine work.

Can C74500-H08 be welded?

With care — weldability is rated fair (40/100). Arc/gas fusion welding is poor because zinc fumes and volatilises; resistance spot/seam welding is good and silver brazing or soldering is excellent — use ventilation and low-zinc filler when fusion joining is unavoidable.

What surface finishes work on C74500-H08?

Takes a bright white mirror polish directly and is a standard base for nickel, chrome, silver or gold plating; lacquer or clear coat outdoors to prevent slow tarnish — cannot be anodized.

Can C74500-H08 be formed, bent or molded?

Excellent cold formability in O61/H01 (deep drawing, spinning, coining); interanneal ~600–700 °C, and stress-relieve cold-worked parts at ~250–300 °C to avoid ammonia-related stress-corrosion cracking.

What is the maximum service temperature of C74500-H08?

C74500-H08 is rated for continuous use to about 140°C (284 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C74500-H02 and C74500-H10?

H02 is the default condition — the general-purpose stocked strip temper: good balance of strength, flatness and forming for hardware and decorative parts. H10: maximum-strength cold-rolled strip for highly stressed flat springs; essentially no formability. Yield strength is 400 MPa in H02 versus 675 MPa in H10.

Sources

  1. ASTM B122/B122M — Copper-Nickel-Zinc (Nickel Silver) Plate, Sheet, Strip and Rolled Bar — ASTM International (2022)
  2. ASTM B151/B151M — Copper-Nickel-Zinc and Copper-Nickel Rod and Bar — ASTM International (2021)
  3. CDA Alloy Database — C74500 property sheet — Copper Development Association (2023)
  4. 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.