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Copper Alloy C17510-TH04

Precip hard

UNS C17510 · ASTM B441 · EN CW110C

TH04 = tD04 and precipitation hardened

C17510 cold worked to full hard before ageing, giving the peak strength and hardness of the alloy while keeping ~45–55 % IACS conductivity, at the cost of low ductility.

CNC machiningSheet metalSpecialty cost $$$$$

Values for the TH04 condition

Other C17510 tempers and conditions

C17510 is listed in 8 conditions; see the grade overview at C17510.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
ADefault
Solution annealed
Pick for maximum formability/machining of complex shapes before customer age-hardening.1703102570 HB22 % IACS
Solution heat treated and cold worked, half hard
Cold-worked stock used when a moderate strength increase after subsequent ageing is wanted.41550012130 HB22 % IACS
Solution heat treated and cold worked, full hard
Fully cold-drawn unaged rod/wire; ages to the highest strength (TH04).5005708150 HB21 % IACS
Mill hardened, half hard
Strip/plate supplied already aged by the mill for form-and-use parts where in-house heat treatment is impractical.5506901513 HRC48 % IACS
solution annealed then precipitation aged
Standard age-hardened condition for machined parts: high conductivity with 690–830 MPa strength and low residual stress.6207251522 HRC50 % IACS
TD02 and precipitation hardened
Compromise between AT and TH04: higher strength than AT with more ductility than fully hard aged.6907951225 HRC48 % IACS
Hardened
Highest strength condition of C17510 — pick for welding electrode holders, dies and high-load conductive springs.7258301028 HRC50 % IACS
TH04This page
TD04 and precipitation hardened
C17510 cold worked to full hard before ageing, giving the peak strength and hardness of the alloy while keeping ~45–55 % IACS conductivity, at the cost of low ductility.760830828 HRC48 % IACS

What is C17510-TH04?

C17510-TH04 is C17510 in the TH04 condition — c17510 cold worked to full hard before ageing, giving the peak strength and hardness of the alloy while keeping ~45–55 % IACS conductivity, at the cost of low ductility. C17510-TH04 has a yield strength of 760 MPa (110 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 98% of copper alloy grades. Elongation at break is 8% and the elastic modulus is 138 GPa (20 Msi). C17510-TH04 has a density of 8.83 g/cm³ (0.319 lb/in³), heavier than 65% of copper alloy grades. It melts at 1,000°C (1,832 °F). A is the default condition FabDigit quotes; TH04 is available on request or by drawing note.

Advantages

  • Tough — resists crack growth — 95 MPa·√m (86.5 ksi·√in), better than 100% of copper alloy grades
  • High strength — 760 MPa (110 ksi), better than 98% of copper alloy grades
  • Stiff — 138 GPa (20 Msi), better than 95% of copper alloy grades
  • High service temperature — 340°C (644 °F), better than 94% of copper alloy grades
  • Conducts heat well — 230 W/m·K (132.9 BTU/hr·ft·°F), better than 81% of copper alloy grades

Limitations

  • High embodied carbon — 6.5 kg CO₂/kg, worse than 94% of copper alloy grades
  • Limited formability — 12/100, worse than 85% of copper alloy grades
  • Limited ductility — 8%, worse than 83% of copper alloy grades

C17510-TH04 properties

Typical room-temperature values for C17510-TH04; 39 are specific to this condition. Other listed values are C17510 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C17510-TH04 has a density of 8.83 g/cm³ (0.319 lb/in³), heavier than 65% of copper alloy grades. It melts at 1,000°C (1,832 °F).

Density8.83 g/cm³0.32 lb/in³
Melting Point (Solidus)1,000°C1,832 °F
Liquidus Temperature1,070°C1,958 °F

Mechanical15

C17510-TH04 has a yield strength of 760 MPa (110 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 98% of copper alloy grades. Elongation at break is 8% and the elastic modulus is 138 GPa (20 Msi).

Elastic (Young's) Modulus138 GPa20 Msi
Shear Modulus53 GPa7.7 Msi
Bulk Modulus115 GPa16.7 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)830 MPa120 ksi
Yield Strength (0.2% offset)760 MPa110 ksi
Elongation at Break8%
Reduction in Area18%
Shear Strength505 MPa73.2 ksi
Fatigue Strength (Endurance Limit)290 MPa42.1 ksi
Fracture Toughness (K_IC)95 MPa·√m86.5 ksi·√in
Charpy V-Notch Impact (RT)60 J44.3 ft·lbf
Hardness, Brinell250 HB
Hardness, Rockwell B100 HRB
Hardness, Vickers275 HV

Thermal5

C17510-TH04 is rated for continuous service to 340°C (644 °F). It conducts heat at 230 W/m·K (132.9 BTU/hr·ft·°F), better than 81% of copper alloy grades. Thermal expansion is 17.6 µm/m·K (9.78 µin/in·°F).

Thermal Conductivity230 W/m·K133 BTU/hr·ft·°F
Specific Heat Capacity420 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)17.6 µm/m·K9.8 µin/in·°F
Max Service Temperature (continuous)340°C644 °F
Min Service Temperature-200°C-328 °F

Electrical3

C17510-TH04 conducts electricity at 48 % IACS, better than 78% of copper alloy grades.

Electrical Conductivity48 % IACS
Electrical Resistivity3.59×10⁻⁸ Ω·m1.41 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)-0.2 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood in fresh and salt water, steam and mild industrial atmospheres; avoid ammonia and oxidizing acids — cold-worked material is more sensitive to stress corrosion.

Sustainability4

Producing a kilogram of C17510-TH04 takes about 90 MJ of energy and emits 6.5 kg of CO₂ — more than 93% of copper alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)90 MJ/kg38,693 BTU/lb
Embodied Carbon (primary production)6.5 kg CO₂/kg
Embodied Water400 L/kg47.9 gal/lb
Typical Recycled Content30%

Manufacturability8

C17510-TH04's machinability is fair (50/100, better than 69% of copper alloy grades); weldability fair (50/100); formability not recommended (12/100).

MachinabilityFair50/100
Machinability Rating (AISI 1212 = 100 %)40%
WeldabilityFair50/100
Formability (cold)Not recommended12/100
CastabilityFair45/100
Brazeability / SolderabilityVery good70/100
PolishabilityVery good82/100
Anodizing Responsen/a — copper alloy, not anodized

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

Working with C17510-TH04

Is C17510 easy to machine?

Machine mainly in the aged condition with sharp carbide tools, positive rake and flood coolant; soft TB00 stock is gummy — always capture beryllium-bearing dust/mist with local exhaust and wet methods.

Can C17510 be welded?

Resistance, GTAW, EBW and laser welding are all practical (use matching or Cu-Ni filler); re-solution-treat and age welds to restore strength, and control fume exposure to Be.

Can C17510 be formed, bent or molded?

Form, bend and coin in the TB00/TD tempers, then age 3 h at ~480 °C (allow for slight growth and springback); avoid severe forming after ageing.

What surface finishes work on C17510?

Not anodizable — bright dip/passivate for a copper finish, or electroless nickel, silver or hard chrome plate for wear/contact surfaces; polishes to a mirror finish in the aged condition.

C17510 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
Beberyllium — precipitation former0.2 – 0.60.35
NiNi (Co may substitute in part per some specs)1.4 – 2.21.9
Coincidental / partial Ni substitute≤ 0.3
Feimpurity limit (typical mill practice)≤ 0.1
CuCu + named elements ≥ 99.5 %balance

C17510-TH04 — frequently asked

What is C17510-TH04 used for?

C17510-TH04 is typically used for resistance spot-welding electrode holders, welding electrode plunger tips, injection mould inserts and cores, high-current spring contacts, connector components and heat-sink and conductive structural parts. In short: spring-tempered copper.

What is the yield strength of C17510-TH04?

C17510-TH04 has a typical yield strength of 760 MPa (110 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 98% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C17510-TH04 easy to machine?

Reasonably — machinability is rated fair (50/100, better than 69% of copper alloy grades). Machine mainly in the aged condition with sharp carbide tools, positive rake and flood coolant; soft TB00 stock is gummy — always capture beryllium-bearing dust/mist with local exhaust and wet methods.

Can C17510-TH04 be welded?

With care — weldability is rated fair (50/100). Resistance, GTAW, EBW and laser welding are all practical (use matching or Cu-Ni filler); re-solution-treat and age welds to restore strength, and control fume exposure to Be.

What surface finishes work on C17510-TH04?

Not anodizable — bright dip/passivate for a copper finish, or electroless nickel, silver or hard chrome plate for wear/contact surfaces; polishes to a mirror finish in the aged condition.

Can C17510-TH04 be formed, bent or molded?

Form, bend and coin in the TB00/TD tempers, then age 3 h at ~480 °C (allow for slight growth and springback); avoid severe forming after ageing.

What is the maximum service temperature of C17510-TH04?

C17510-TH04 is rated for continuous use to about 340°C (644 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C17510-A and C17510-TH04?

A is the default condition — pick for maximum formability/machining of complex shapes before customer age-hardening. TH04: c17510 cold worked to full hard before ageing, giving the peak strength and hardness of the alloy while keeping ~45–55 % IACS conductivity, at the cost of low ductility. Yield strength is 170 MPa in A versus 760 MPa in TH04.

Can FabDigit make parts in C17510-TH04?

Yes — C17510-TH04 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. ASTM B441 — Copper-Cobalt-Beryllium and Copper-Nickel-Beryllium Rod and Bar — ASTM (2019)
  2. ASTM B534 — Copper-Cobalt-Beryllium / Copper-Nickel-Beryllium Plate, Sheet, Strip and Rolled Bar — ASTM (2019)
  3. Materion Alloy 3 (C17510) technical datasheet — Materion Brush Performance Alloys (2022)
  4. C17510 alloy property sheet — Copper Development Association (copper.org) (2021)
  5. 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.