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Copper Alloy C17000-TB00

Heat-treated state

UNS C17000 · EN CW100C

TB00 = solution heat treated

Softest supply condition — deep draw, stamp or form complex parts, then age harden.

High cost $$$$

Values for the TB00 condition

Other C17000 tempers and conditions

C17000 is listed in 14 conditions; see the grade overview at C17000.

Compare all 14 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
TB00This page
Solution heat treated
Softest supply condition — deep draw, stamp or form complex parts, then age harden.24048045110 HB17 % IACS
Solution heat treated and cold worked, quarter hard
Light cold work for parts needing extra stiffness in forming while still bendable before aging.48058528145 HB17 % IACS
Solution heat treated and cold worked, half hard
Half-hard strip/rod for moderate forming with higher as-formed strength before age hardening.57065515185 HB17 % IACS
Mill hardened
Ready-to-use mill hardened strip: no customer aging, best formability of the TM series.6207601622 HRC24 % IACS
Solution heat treated and cold worked, full hard
Fully cold-worked temper for flat springs and contacts that receive only simple bends before aging.690760520 HRC17 % IACS
mill hardened quarter hard
Mill hardened strip balancing forming of moderate bends with mid-level spring strength.6908301425 HRC24 % IACS
Mill hardened, half hard
Common connector-strip temper: no heat treat needed, good stress relaxation resistance.7909001128 HRC24 % IACS
Mill hardened, full hard
Higher-strength mill hardened strip for stamped springs with generous bend radii.860965930 HRC24 % IACS
mill hardened extra hard
Extra-hard mill hardened temper for high-force contacts where only mild forming is required.9301,035733 HRC24 % IACS
TF00Default
Solution heat treated and precipitation hardened
Standard peak-aged bar/rod/plate condition for high-strength machined parts and molds.1,0001,140636 HRC23 % IACS
Mill hardened, extra hard
Strongest mill hardened temper — near TH-level strength with no customer heat treatment.1,0001,105634 HRC24 % IACS
TD01 and precipitation hardened
Formed from TD01 stock and aged — highest strength with some residual ductility.1,0501,180537 HRC23 % IACS
TD02 and precipitation hardened
Aged half-hard strip for springs needing high yield strength and good fatigue life.1,0851,220438 HRC23 % IACS
TD04 and precipitation hardened
Maximum-strength condition for flat springs, diaphragms and contact fingers with simple geometry.1,1201,255339 HRC23 % IACS

What is C17000-TB00?

C17000-TB00 is C17000 heat treated to TB00 — softest supply condition — deep draw, stamp or form complex parts, then age harden. C17000-TB00 has a yield strength of 240 MPa (34.8 ksi) and a tensile strength of 480 MPa (69.6 ksi) — stronger than 52% of copper alloy grades. Elongation at break is 45% and the elastic modulus is 128 GPa (18.6 Msi). C17000-TB00 has a density of 8.41 g/cm³ (0.304 lb/in³), lighter than 72% of copper alloy grades. It melts at 866°C (1,591 °F). TF00 is the default condition FabDigit quotes; TB00 is available on request or by drawing note.

Advantages

  • Polishes to a fine finish — 85/100, better than 92% of copper alloy grades
  • Ductile — tolerates forming and impact — 45%, better than 91% of copper alloy grades
  • Forms and bends easily — 90/100, better than 89% of copper alloy grades

Limitations

  • Limited service temperature — 150°C (302 °F), worse than 96% of copper alloy grades
  • High embodied carbon — 6.5 kg CO₂/kg, worse than 94% of copper alloy grades
  • Difficult to machine — 25/100, worse than 86% of copper alloy grades

C17000-TB00 properties

Typical room-temperature values for C17000-TB00; 15 are specific to this condition. Other listed values are C17000 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C17000-TB00 has a density of 8.41 g/cm³ (0.304 lb/in³), lighter than 72% of copper alloy grades. It melts at 866°C (1,591 °F).

Density8.41 g/cm³0.3 lb/in³
Melting Point (Solidus)866°C1,591 °F
Liquidus Temperature980°C1,796 °F

Mechanical16

C17000-TB00 has a yield strength of 240 MPa (34.8 ksi) and a tensile strength of 480 MPa (69.6 ksi) — stronger than 52% of copper alloy grades. Elongation at break is 45% and the elastic modulus is 128 GPa (18.6 Msi).

Elastic (Young's) Modulus128 GPa18.6 Msi
Shear Modulus50 GPa7.3 Msi
Bulk Modulus115 GPa16.7 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)480 MPa69.6 ksi
Yield Strength (0.2% offset)240 MPa34.8 ksi
Elongation at Break45%
Reduction in Area20%
Compressive Strength1,100 MPa160 ksi
Shear Strength330 MPa47.9 ksi
Fatigue Strength (Endurance Limit)190 MPa27.6 ksi
Fracture Toughness (K_IC)45 MPa·√m41 ksi·√in
Charpy V-Notch Impact (RT)12 J8.9 ft·lbf
Hardness, Brinell110 HB
Hardness, Rockwell C36 HRC
Hardness, Vickers355 HV

Thermal6

C17000-TB00 is rated for continuous service to 150°C (302 °F). It conducts heat at 84 W/m·K (48.5 BTU/hr·ft·°F), better than 51% of copper alloy grades. Thermal expansion is 17 µm/m·K (9.44 µin/in·°F).

Thermal Conductivity84 W/m·K48.5 BTU/hr·ft·°F
Specific Heat Capacity420 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)17 µm/m·K9.4 µin/in·°F
Latent Heat of Fusion200 J/g86 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-200°C-328 °F

Electrical3

C17000-TB00 conducts electricity at 17 % IACS, better than 50% of copper alloy grades.

Electrical Conductivity17 % IACS
Electrical Resistivity1.01×10⁻⁷ Ω·m3.98 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (70/100), better than 76% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.2 V
Corrosion ResistanceVery good70/100
Chemical Resistance SummaryGood in seawater, industrial atmospheres and non-oxidizing acids; attacked by ammonia/amines (stress-corrosion risk), nitric acid, and strongly oxidizing media; sulfide environments tarnish the surface.

Sustainability4

Producing a kilogram of C17000-TB00 takes about 95 MJ of energy and emits 6.5 kg of CO₂ — more than 95% of copper alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)95 MJ/kg40,843 BTU/lb
Embodied Carbon (primary production)6.5 kg CO₂/kg
Embodied Water260 L/kg31.2 gal/lb
Typical Recycled Content30%

Manufacturability8

C17000-TB00's machinability is poor (25/100, worse than 86% of copper alloy grades); weldability fair (50/100); formability excellent (90/100).

MachinabilityPoor25/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityFair50/100
Formability (cold)Excellent90/100
CastabilityFair45/100
Brazeability / SolderabilityVery good70/100
PolishabilityExcellent85/100
Anodizing Responsen/a — copper alloy; use nickel/gold/silver electroplating or passivation instead of anodizing

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

Working with C17000-TB00

Is C17000 easy to machine?

Machine in the aged (TF00/TH) condition with sharp carbide tools, positive rake and flood coolant; capture all chips/dust — beryllium-bearing particulate requires local exhaust and no dry grinding.

Can C17000 be welded?

Resistance, electron-beam and laser welding are preferred; GTAW is possible with matching filler but the weld zone softens and must be re-solution treated and aged; ventilate fumes.

Can C17000 be formed, bent or molded?

Form in TB00 or TD tempers before precipitation aging (typically ~315–330 °C for 2–3 h); aged material has limited bend ductility and springback is high.

What surface finishes work on C17000?

Takes a high mirror polish for mold inserts; electroless nickel, nickel/gold or silver plating is common for contacts; avoid ammonia-based cleaners to prevent stress-corrosion cracking.

C17000 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
Be1.6 – 1.791.7
Co+Niminimum combined cobalt + nickel≥ 0.20.3
Co+Ni+Femaximum combined≤ 0.6—
Curemainder, including listed additionsbalance—

C17000-TB00 — frequently asked

What is C17000-TB00 used for?

C17000-TB00 is typically used for springs, relay and switch parts and electrical connectors. In short: high-strength beryllium copper; 1000 MPa yield after aging; formable before age hardening.

What is the yield strength of C17000-TB00?

C17000-TB00 has a typical yield strength of 240 MPa (34.8 ksi) and a tensile strength of 480 MPa (69.6 ksi) — stronger than 52% of copper alloy grades. Strength varies by condition: see the 14 listed tempers.

Is C17000-TB00 easy to machine?

Not especially — machinability is rated poor (25/100, worse than 86% of copper alloy grades). Machine in the aged (TF00/TH) condition with sharp carbide tools, positive rake and flood coolant; capture all chips/dust — beryllium-bearing particulate requires local exhaust and no dry grinding.

Can C17000-TB00 be welded?

With care — weldability is rated fair (50/100). Resistance, electron-beam and laser welding are preferred; GTAW is possible with matching filler but the weld zone softens and must be re-solution treated and aged; ventilate fumes.

What surface finishes work on C17000-TB00?

Takes a high mirror polish for mold inserts; electroless nickel, nickel/gold or silver plating is common for contacts; avoid ammonia-based cleaners to prevent stress-corrosion cracking.

Can C17000-TB00 be formed, bent or molded?

Form in TB00 or TD tempers before precipitation aging (typically ~315–330 °C for 2–3 h); aged material has limited bend ductility and springback is high.

What is the maximum service temperature of C17000-TB00?

C17000-TB00 is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C17000-TF00 and C17000-TB00?

TF00 is the default condition — standard peak-aged bar/rod/plate condition for high-strength machined parts and molds. TB00: softest supply condition — deep draw, stamp or form complex parts, then age harden. Yield strength is 1,000 MPa in TF00 versus 240 MPa in TB00.

Sources

  1. ASTM B194 / B196 / B197 — Beryllium copper strip, rod and wire — ASTM International (2020)
  2. CDA Alloy C17000 property datasheet — Copper Development Association (2023)
  3. Alloy 165 (C17000) technical data — Materion Brush Performance Alloys (2022)
  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.