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Copper Alloy C17465-TD02

Supply condition

UNS C17465

TD02 = solution heat treated and cold worked, half hard

Intermediate stiffness/strength for parts that still need some bending before aging.

High cost $$$$

Values for the TD02 condition

Other C17465 tempers and conditions

C17465 is listed in 6 conditions; see the grade overview at C17465.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution heat treated
Softest, most formable condition — pick when parts are deep-formed or heavily machined before age hardening.1603302890 HB28 % IACS
TD02This page
Solution heat treated and cold worked, half hard
Intermediate stiffness/strength for parts that still need some bending before aging.37045012130 HB30 % IACS
Solution heat treated and cold worked, full hard
Cold-drawn rod/strip used where the part will be aged after machining, or where moderate strength without heat treatment is enough.4805408160 HB32 % IACS
TF00Default
Solution heat treated and precipitation hardened
Standard stocked rod condition: near-isotropic aged properties with high conductivity, best for machined electrode and contact parts.5506901522 HRC50 % IACS
TD02 and precipitation hardened
Compromise between the ductility of TF00 and the peak strength of TH04 for formed-then-aged components.6207251224 HRC50 % IACS
TD04 and precipitation hardened
Peak-strength condition for small-diameter rod, springs and highly loaded contacts that still need ~50 % IACS.690760928 HRC52 % IACS

What is C17465-TD02?

C17465-TD02 is C17465 supplied in the TD02 condition — intermediate stiffness/strength for parts that still need some bending before aging. C17465-TD02 has a yield strength of 370 MPa (53.7 ksi) and a tensile strength of 450 MPa (65.3 ksi) — stronger than 75% of copper alloy grades. Elongation at break is 12% and the elastic modulus is 132 GPa (19.1 Msi). C17465-TD02 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). TF00 is the default condition FabDigit quotes; TD02 is available on request or by drawing note.

Advantages

  • Stiff — 132 GPa (19.1 Msi), better than 93% of copper alloy grades
  • High strength — 370 MPa (53.7 ksi), better than 75% of copper alloy grades

Limitations

  • High embodied carbon — 6.5 kg CO₂/kg, worse than 94% of copper alloy grades
  • Difficult to weld — 25/100, worse than 78% of copper alloy grades

C17465-TD02 properties

Typical room-temperature values for C17465-TD02; 21 are specific to this condition. Other listed values are C17465 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C17465-TD02 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

Mechanical16

C17465-TD02 has a yield strength of 370 MPa (53.7 ksi) and a tensile strength of 450 MPa (65.3 ksi) — stronger than 75% of copper alloy grades. Elongation at break is 12% and the elastic modulus is 132 GPa (19.1 Msi).

Elastic (Young's) Modulus132 GPa19.1 Msi
Shear Modulus53 GPa7.7 Msi
Bulk Modulus115 GPa16.7 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)450 MPa65.3 ksi
Yield Strength (0.2% offset)370 MPa53.7 ksi
Elongation at Break12%
Reduction in Area35%
Compressive Strength380 MPa55.1 ksi
Shear Strength305 MPa44.2 ksi
Fatigue Strength (Endurance Limit)180 MPa26.1 ksi
Charpy V-Notch Impact (RT)38 J28 ft·lbf
Hardness, Brinell130 HB
Hardness, Rockwell B72 HRB
Hardness, Rockwell C22 HRC
Hardness, Vickers140 HV

Thermal6

C17465-TD02 is rated for continuous service to 200°C (392 °F). It conducts heat at 135 W/m·K (78 BTU/hr·ft·°F), better than 71% of copper alloy grades. Thermal expansion is 17.6 µm/m·K (9.78 µin/in·°F).

Thermal Conductivity135 W/m·K78 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
Latent Heat of Fusion205 J/g88.1 BTU/lb
Max Service Temperature (continuous)200°C392 °F
Min Service Temperature-200°C-328 °F

Electrical3

C17465-TD02 conducts electricity at 30 % IACS, better than 71% of copper alloy grades.

Electrical Conductivity30 % IACS
Electrical Resistivity5.75×10⁻⁸ Ω·m2.26 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/sea water, steam and most neutral salts; attacked by ammonia and amines (stress corrosion), oxidising acids, sulphides and mercury compounds; lead phase can leach in potable-water service.

Sustainability4

Producing a kilogram of C17465-TD02 takes about 100 MJ of energy and emits 6.5 kg of CO₂ — more than 96% of copper alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)100 MJ/kg42,992 BTU/lb
Embodied Carbon (primary production)6.5 kg CO₂/kg
Embodied Water260 L/kg31.2 gal/lb
Typical Recycled Content30%

Manufacturability8

C17465-TD02's machinability is good (58/100, better than 73% of copper alloy grades); weldability poor (25/100); formability fair (50/100).

MachinabilityGood58/100
Machinability Rating (AISI 1212 = 100 %)50%
WeldabilityPoor25/100
Formability (cold)Fair50/100
CastabilityFair45/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper alloy; use tin, silver or nickel plating instead

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

Working with C17465-TD02

Is C17465 easy to machine?

Lead addition gives short chips and good surface finish — turn dry or with flood coolant at BeCu speeds, and capture all dust/fines under local exhaust because beryllium particulate is hazardous.

Can C17465 be welded?

Fusion welding is unreliable (lead-induced hot cracking); use resistance or electron-beam joining on unleaded transition pieces, or mechanical/brazed joints.

Can C17465 be formed, bent or molded?

Form only in TB00/TD02; aged tempers have limited bend ductility — age after forming (typically ~480 °C, 2–3 h) with allowance for slight growth.

What surface finishes work on C17465?

Not anodizable; electroless nickel, silver or tin plating are standard, and the aged alloy polishes to a bright, wear-resistant surface.

C17465 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
Beprecipitation hardening element0.15 – 0.50.3
Niforms NiBe precipitates1 – 1.41.2
Pbfree-machining addition0.2 – 0.60.4
CuCu + named elements 99.5 % minbalance—

C17465-TD02 — frequently asked

What is C17465-TD02 used for?

C17465-TD02 is typically used for connectors, precision bushings and molds. In short: free-machining beryllium copper; 50 % IACS at 550 MPa; 300 °C service ceiling.

What is the yield strength of C17465-TD02?

C17465-TD02 has a typical yield strength of 370 MPa (53.7 ksi) and a tensile strength of 450 MPa (65.3 ksi) — stronger than 75% of copper alloy grades. Strength varies by condition: see the 6 listed tempers.

Is C17465-TD02 easy to machine?

Reasonably — machinability is rated good (58/100, better than 73% of copper alloy grades). Lead addition gives short chips and good surface finish — turn dry or with flood coolant at BeCu speeds, and capture all dust/fines under local exhaust because beryllium particulate is hazardous.

Can C17465-TD02 be welded?

Not readily — weldability is rated poor (25/100). Fusion welding is unreliable (lead-induced hot cracking); use resistance or electron-beam joining on unleaded transition pieces, or mechanical/brazed joints.

What surface finishes work on C17465-TD02?

Not anodizable; electroless nickel, silver or tin plating are standard, and the aged alloy polishes to a bright, wear-resistant surface.

Can C17465-TD02 be formed, bent or molded?

Form only in TB00/TD02; aged tempers have limited bend ductility — age after forming (typically ~480 °C, 2–3 h) with allowance for slight growth.

What is the maximum service temperature of C17465-TD02?

C17465-TD02 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 C17465-TF00 and C17465-TB00?

TF00 is the default condition — standard stocked rod condition: near-isotropic aged properties with high conductivity, best for machined electrode and contact parts. TB00: softest, most formable condition — pick when parts are deep-formed or heavily machined before age hardening. Yield strength is 550 MPa in TF00 versus 160 MPa in TB00.

Sources

  1. ASTM B441 / B534 — Cu-Ni-Be rod, bar and plate — ASTM International (2020)
  2. CDA Copper Alloy Database — C17460 / C17465 — Copper Development Association (2023)
  3. High-conductivity beryllium copper (Alloy 3 / Alloy 174) data — Materion Brush Performance Alloys (2022)
  4. ASM Handbook Vol. 2 — Properties of Copper and Copper 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.