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Copper Alloy C18200-TH01

Precip hard

UNS C18200 · ASTM B624 · EN CuCr1, CW105C · JIS C1820

TH01 = tD01 and precipitation hardened

Moderate cold work plus aging: good balance of formed-part strength and conductivity in strip/rod.

Values for the TH01 condition

Other C18200 tempers and conditions

C18200 is listed in 8 conditions; see the grade overview at C18200.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution heat treated
Pick when heavy cold forming, deep drawing or machining of complex shapes is needed before a final aging cycle.962344055 HB42 % IACS
Solution heat treated and cold worked, full hard
Cold-worked strength without the aging step; choose when conductivity is secondary and a later age-hardening cycle will follow.36040012120 HB45 % IACS
Solution heat treated and precipitation hardened
Best choice for large sections, forgings and mould inserts where uniform properties and high conductivity matter more than peak strength.37244822120 HB82 % IACS
TH01This page
TD01 and precipitation hardened
Moderate cold work plus aging: good balance of formed-part strength and conductivity in strip/rod.40047620130 HB82 % IACS
Cold worked and stress-relieved rod/wire
Drawn and stress-relieved condition for straight, dimensionally stable rod and wire where full aging response is not specified.41047014130 HB78 % IACS
TD02 and precipitation hardened
Half-hard + aged temper for switch arms, holders and contact supports needing spring-like stiffness with high conductivity.42749618140 HB82 % IACS
HDefault
Hardened
Standard stocked condition for electrode bar and rod: ~75–80 HRB with ≥80% IACS.43050018140 HB82 % IACS
TD04 and precipitation hardened
Highest strength/hardness combination for resistance-welding electrodes, shanks and heavy-duty conductors.44851716145 HB81 % IACS

What is C18200-TH01?

C18200-TH01 is C18200 in the TH01 condition — moderate cold work plus aging: good balance of formed-part strength and conductivity in strip/rod. C18200-TH01 has a yield strength of 400 MPa (58 ksi) and a tensile strength of 476 MPa (69 ksi) — stronger than 80% of copper alloy grades. Elongation at break is 20% and the elastic modulus is 117 GPa (17 Msi). C18200-TH01 has a density of 8.89 g/cm³ (0.321 lb/in³), heavier than 72% of copper alloy grades. It melts at 1,070°C (1,958 °F). H is the default condition FabDigit quotes; TH01 is available on request or by drawing note.

Advantages

  • High service temperature — 400°C (752 °F), better than 97% of copper alloy grades
  • High electrical conductivity — 82 % IACS, better than 85% of copper alloy grades
  • Conducts heat well — 320 W/m·K (184.9 BTU/hr·ft·°F), better than 84% of copper alloy grades
  • High strength — 400 MPa (58 ksi), better than 80% of copper alloy grades

C18200-TH01 properties

Typical room-temperature values for C18200-TH01; 20 are specific to this condition. Other listed values are C18200 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C18200-TH01 has a density of 8.89 g/cm³ (0.321 lb/in³), heavier than 72% of copper alloy grades. It melts at 1,070°C (1,958 °F).

Density8.89 g/cm³0.32 lb/in³
Melting Point (Solidus)1,070°C1,958 °F
Liquidus Temperature1,080°C1,976 °F

Mechanical12

C18200-TH01 has a yield strength of 400 MPa (58 ksi) and a tensile strength of 476 MPa (69 ksi) — stronger than 80% of copper alloy grades. Elongation at break is 20% and the elastic modulus is 117 GPa (17 Msi).

Elastic (Young's) Modulus117 GPa17 Msi
Shear Modulus44 GPa6.4 Msi
Bulk Modulus133 GPa19.3 Msi
Poisson's Ratio0.34
Tensile Strength (Ultimate)476 MPa69 ksi
Yield Strength (0.2% offset)400 MPa58 ksi
Elongation at Break20%
Shear Strength300 MPa43.5 ksi
Fatigue Strength (Endurance Limit)165 MPa23.9 ksi
Hardness, Brinell130 HB
Hardness, Rockwell B72 HRB
Hardness, Vickers137 HV

Thermal6

C18200-TH01 is rated for continuous service to 400°C (752 °F). It conducts heat at 320 W/m·K (184.9 BTU/hr·ft·°F), better than 84% of copper alloy grades. Thermal expansion is 17.6 µm/m·K (9.78 µin/in·°F).

Thermal Conductivity320 W/m·K185 BTU/hr·ft·°F
Specific Heat Capacity385 J/kg·K0.09 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)400°C752 °F
Min Service Temperature-200°C-328 °F

Electrical3

C18200-TH01 conducts electricity at 82 % IACS, better than 85% of copper alloy grades.

Electrical Conductivity82 % IACS
Electrical Resistivity2.1×10⁻⁸ Ω·m0.827 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)-0.3 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood in fresh/industrial atmospheres, fresh water and non-oxidising acids; attacked by ammonia and amines (stress corrosion), oxidising acids, and rapidly tarnished/oxidised above ~200 °C in air.

Sustainability4

Producing a kilogram of C18200-TH01 takes about 57 MJ of energy and emits 3.5 kg of CO₂ — less than 52% of copper alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)57 MJ/kg24,506 BTU/lb
Embodied Carbon (primary production)3.5 kg CO₂/kg
Embodied Water350 L/kg41.9 gal/lb
Typical Recycled Content30%

Manufacturability7

C18200-TH01's machinability is fair (40/100, better than 57% of copper alloy grades); weldability poor (30/100); formability fair (40/100).

MachinabilityFair40/100
Machinability Rating (AISI 1212 = 100 %)60%
WeldabilityPoor30/100
Formability (cold)Fair40/100
Brazeability / SolderabilityVery good75/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper alloy; use tin/nickel/silver plating or bare oxidised finish

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

Working with C18200-TH01

Is C18200 easy to machine?

Machine in the aged (TH/TF) condition with sharp positive-rake carbide, high speed and generous coolant; gummy and prone to built-up edge when solution treated.

Can C18200 be welded?

Fusion welding is poor — Cr oxide films and hot cracking; prefer brazing, silver soldering or mechanical/threaded joints, and re-age locally softened zones.

Can C18200 be formed, bent or molded?

Form, bend or upset in TB00 (soft) condition then age 450–500 °C for 2–4 h; cold formability drops sharply once aged.

What surface finishes work on C18200?

Not anodizable; use bright turning/polishing, chemical bright dip, or nickel/silver/tin plating for contact surfaces and tarnish resistance.

C18200 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
Crprimary precipitation-hardening addition0.6 – 1.20.9
Feimpurity limit≤ 0.10.03
Siimpurity limit≤ 0.10.02
Pbimpurity limit≤ 0.050.01
CuCu + named elements ≥ 99.5 % (Ag countable as Cu)≥ 98.6 (balance)—

C18200-TH01 — frequently asked

What is C18200-TH01 used for?

C18200-TH01 is typically used for resistance spot-welding electrodes (RWMA Class 2), electrode holders and shanks, switch and breaker contact arms, continuous-casting mould components, injection mould inserts and high-current bus conductors. In short: high-temp conductivity.

What is the yield strength of C18200-TH01?

C18200-TH01 has a typical yield strength of 400 MPa (58 ksi) and a tensile strength of 476 MPa (69 ksi) — stronger than 80% of copper alloy grades. Strength varies by condition: see the 8 listed tempers.

Is C18200-TH01 easy to machine?

Not especially — machinability is rated fair (40/100, better than 57% of copper alloy grades). Machine in the aged (TH/TF) condition with sharp positive-rake carbide, high speed and generous coolant; gummy and prone to built-up edge when solution treated.

Can C18200-TH01 be welded?

Not readily — weldability is rated poor (30/100). Fusion welding is poor — Cr oxide films and hot cracking; prefer brazing, silver soldering or mechanical/threaded joints, and re-age locally softened zones.

What surface finishes work on C18200-TH01?

Not anodizable; use bright turning/polishing, chemical bright dip, or nickel/silver/tin plating for contact surfaces and tarnish resistance.

Can C18200-TH01 be formed, bent or molded?

Form, bend or upset in TB00 (soft) condition then age 450–500 °C for 2–4 h; cold formability drops sharply once aged.

What is the maximum service temperature of C18200-TH01?

C18200-TH01 is rated for continuous use to about 400°C (752 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C18200-H and C18200-TB00?

H is the default condition — standard stocked condition for electrode bar and rod: ~75–80 HRB with ≥80% IACS. TB00: pick when heavy cold forming, deep drawing or machining of complex shapes is needed before a final aging cycle. Yield strength is 430 MPa in H versus 96 MPa in TB00.

Can FabDigit make parts in C18200-TH01?

Yes — C18200-TH01 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 B224 — Standard Classification of Coppers — ASTM International (2021)
  2. ASTM B601 — Temper Designations for Copper and Copper Alloys — ASTM International (2019)
  3. RWMA Bulletin 16 — Resistance Welding Electrode Classification (Class 2) — AWS/RWMA (2017)
  4. UNS C18200 alloy datasheet — Copper Development Association (copper.org) (2023)
  5. ASM Handbook Vol.2 — Properties of 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.