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Copper Alloy C17510-TH02

Precip hard

UNS C17510 · ASTM B441 · EN CW110C

TH02 = tD02 and precipitation hardened

Compromise between AT and TH04: higher strength than AT with more ductility than fully hard aged.

CNC machiningSheet metalSpecialty cost $$$$$

Values for the TH02 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
TH02This page
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
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-TH02?

C17510-TH02 is C17510 in the TH02 condition — compromise between AT and TH04: higher strength than AT with more ductility than fully hard aged. C17510-TH02 has a yield strength of 690 MPa (100 ksi) and a tensile strength of 795 MPa (115 ksi) — stronger than 96% of copper alloy grades. Elongation at break is 12% and the elastic modulus is 138 GPa (20 Msi). C17510-TH02 has a density of 8.75 g/cm³ (0.316 lb/in³), lighter than 51% of copper alloy grades. It melts at 1,000°C (1,832 °F). A is the default condition FabDigit quotes; TH02 is available on request or by drawing note.

Advantages

  • High strength — 690 MPa (100 ksi), better than 96% of copper alloy grades
  • Stiff — 138 GPa (20 Msi), better than 95% of copper alloy grades
  • Tough — resists crack growth — 65 MPa·√m (59.2 ksi·√in), better than 95% of copper alloy grades
  • High service temperature — 350°C (662 °F), better than 95% 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 — 4.6 kg CO₂/kg, worse than 82% of copper alloy grades

C17510-TH02 properties

Typical room-temperature values for C17510-TH02; 22 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-TH02 has a density of 8.75 g/cm³ (0.316 lb/in³), lighter than 51% of copper alloy grades. It melts at 1,000°C (1,832 °F).

Density8.75 g/cm³0.32 lb/in³
Melting Point (Solidus)1,000°C1,832 °F
Liquidus Temperature1,070°C1,958 °F

Mechanical15

C17510-TH02 has a yield strength of 690 MPa (100 ksi) and a tensile strength of 795 MPa (115 ksi) — stronger than 96% of copper alloy grades. Elongation at break is 12% 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)795 MPa115 ksi
Yield Strength (0.2% offset)690 MPa100 ksi
Elongation at Break12%
Reduction in Area35%
Shear Strength500 MPa72.5 ksi
Fatigue Strength (Endurance Limit)300 MPa43.5 ksi
Fracture Toughness (K_IC)65 MPa·√m59.2 ksi·√in
Charpy V-Notch Impact (RT)24 J17.7 ft·lbf
Hardness, Brinell230 HB
Hardness, Rockwell B97 HRB
Hardness, Vickers248 HV

Thermal5

C17510-TH02 is rated for continuous service to 350°C (662 °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 Capacity418 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)350°C662 °F
Min Service Temperature-200°C-328 °F

Electrical3

C17510-TH02 conducts electricity at 48 % IACS, better than 78% of copper alloy grades.

Electrical Conductivity48 % IACS
Electrical Resistivity3.6×10⁻⁸ Ω·m1.42 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (65/100), better than 58% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.2 V
Corrosion ResistanceGood65/100
Chemical Resistance SummaryGood in fresh/salt water, steam and non-oxidizing acids; attacked by ammonia/amines (SCC risk), nitric acid, ferric salts and strong oxidizers; tarnishes in sulphur-bearing air.

Sustainability4

Producing a kilogram of C17510-TH02 takes about 65 MJ of energy and emits 4.6 kg of CO₂ — more than 81% of copper alloy grades. Typical recycled content is 25%.

Embodied Energy (primary production)65 MJ/kg27,945 BTU/lb
Embodied Carbon (primary production)4.6 kg CO₂/kg
Embodied Water250 L/kg30 gal/lb
Typical Recycled Content25%

Manufacturability8

C17510-TH02's machinability is fair (42/100, better than 59% of copper alloy grades); weldability good (55/100); formability poor (25/100).

MachinabilityFair42/100
Machinability Rating (AISI 1212 = 100 %)30%
WeldabilityGood55/100
Formability (cold)Poor25/100
CastabilityFair45/100
Brazeability / SolderabilityVery good70/100
PolishabilityVery good80/100
Anodizing Responsen/a — copper alloy; use bright dipping, passivation, electroless Ni or hard chrome instead

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

Working with C17510-TH02

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-TH02 — frequently asked

What is C17510-TH02 used for?

C17510-TH02 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-TH02?

C17510-TH02 has a typical yield strength of 690 MPa (100 ksi) and a tensile strength of 795 MPa (115 ksi) — stronger than 96% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C17510-TH02 easy to machine?

Not especially — machinability is rated fair (42/100, better than 59% 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-TH02 be welded?

Yes — weldability is rated good (55/100). 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-TH02?

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-TH02 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-TH02?

C17510-TH02 is rated for continuous use to about 350°C (662 °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-TH02?

Yes — C17510-TH02 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.