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Copper Alloy C62500-TQ50

Supply condition

UNS C62500 · ASTM B150

TQ50 = quench hardened

Water-quenched from the beta field to give martensitic β′ — maximum hardness for dies, forming tools and wear plates; very brittle, machine before hardening.

High cost $$$$

Values for the TQ50 condition

Other C62500 tempers and conditions

C62500 is listed in 6 conditions; see the grade overview at C62500.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Slow-cooled anneal used to soften material for machining or stress relief before final quench hardening; lowest strength and still low ductility.340620313 HRC8.5 % IACS
As hot forged and air cooled
Choose for near-net forged dies, wear rings and heavy sections where extruded stock sizes are unavailable.400740321 HRC8 % IACS
M30Default
As hot extruded
Standard stocked condition for C62500 rod and bar; good balance of hardness and availability, machine then use as-is.415760222 HRC8 % IACS
Quench hardened and temper annealed
Quench plus temper anneal (typically 400–650 °C) to trade some hardness for toughness and dimensional stability in wear parts and bearings.480790330 HRC7.5 % IACS
Full hard
Light cold draw or sizing pass on small-diameter rod for tighter tolerance and straightness; only small reductions are possible with 13% Al.5008001.525 HRC7.5 % IACS
TQ50This page
Quench hardened
Water-quenched from the beta field to give martensitic β′ — maximum hardness for dies, forming tools and wear plates; very brittle, machine before hardening.550830137 HRC7 % IACS

What is C62500-TQ50?

C62500-TQ50 is C62500 supplied in the TQ50 condition — water-quenched from the beta field to give martensitic β′ — maximum hardness for dies, forming tools and wear plates; very brittle, machine before hardening. C62500-TQ50 has a yield strength of 550 MPa (79.8 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 92% of copper alloy grades. Elongation at break is 1% and the elastic modulus is 114 GPa (16.5 Msi). C62500-TQ50 has a density of 7.16 g/cm³ (0.259 lb/in³), lighter than 100% of copper alloy grades. It melts at 1,035°C (1,895 °F). M30 is the default condition FabDigit quotes; TQ50 is available on request or by drawing note.

Advantages

  • Lightweight — 7.16 g/cm³ (0.259 lb/in³), better than 100% of copper alloy grades
  • High strength — 550 MPa (79.8 ksi), better than 92% of copper alloy grades

Limitations

  • Difficult to machine — 14/100, worse than 100% of copper alloy grades
  • Limited formability — 3/100, worse than 100% of copper alloy grades
  • Limited ductility — 1%, worse than 99% of copper alloy grades
  • Difficult to weld — 12/100, worse than 96% of copper alloy grades
  • Low electrical conductivity — 7 % IACS, worse than 86% of copper alloy grades

C62500-TQ50 properties

Typical room-temperature values for C62500-TQ50; 22 are specific to this condition. Other listed values are C62500 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C62500-TQ50 has a density of 7.16 g/cm³ (0.259 lb/in³), lighter than 100% of copper alloy grades. It melts at 1,035°C (1,895 °F).

Density7.16 g/cm³0.26 lb/in³
Melting Point (Solidus)1,035°C1,895 °F
Liquidus Temperature1,050°C1,922 °F

Mechanical16

C62500-TQ50 has a yield strength of 550 MPa (79.8 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 92% of copper alloy grades. Elongation at break is 1% and the elastic modulus is 114 GPa (16.5 Msi).

Elastic (Young's) Modulus114 GPa16.5 Msi
Shear Modulus43 GPa6.2 Msi
Bulk Modulus105 GPa15.2 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)830 MPa120 ksi
Yield Strength (0.2% offset)550 MPa79.8 ksi
Elongation at Break1%
Reduction in Area2%
Compressive Strength1,050 MPa152 ksi
Shear Strength520 MPa75.4 ksi
Fatigue Strength (Endurance Limit)280 MPa40.6 ksi
Charpy V-Notch Impact (RT)3 J2.2 ft·lbf
Hardness, Brinell340 HB
Hardness, Rockwell B99 HRB
Hardness, Rockwell C37 HRC
Hardness, Vickers360 HV

Thermal6

C62500-TQ50 is rated for continuous service to 250°C (482 °F). It conducts heat at 38 W/m·K (22 BTU/hr·ft·°F), worse than 84% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity38 W/m·K22 BTU/hr·ft·°F
Specific Heat Capacity375 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.2 µm/m·K9 µin/in·°F
Latent Heat of Fusion210 J/g90.3 BTU/lb
Max Service Temperature (continuous)250°C482 °F
Min Service Temperature-200°C-328 °F

Electrical3

C62500-TQ50 conducts electricity at 7 % IACS, worse than 86% of copper alloy grades.

Electrical Conductivity7 % IACS
Electrical Resistivity2.46×10⁻⁷ Ω·m9.69 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is good (66/100), better than 64% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.27 V
Corrosion ResistanceGood66/100
Chemical Resistance SummaryProtective Al₂O₃ film gives good resistance to seawater, brines, dilute non-oxidising acids, alkalis and many organics; attacked by oxidising acids (nitric), ammonia/amines and moist chlorine, and susceptible to dealuminification in stagnant or low-pH chloride service.

Sustainability4

Producing a kilogram of C62500-TQ50 takes about 62 MJ of energy and emits 3.9 kg of CO₂ — more than 76% of copper alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)62 MJ/kg26,655 BTU/lb
Embodied Carbon (primary production)3.9 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content35%

Manufacturability8

C62500-TQ50's machinability is not recommended (14/100, worse than 100% of copper alloy grades); weldability not recommended (12/100); formability not recommended (3/100).

MachinabilityNot recommended14/100
Machinability Rating (AISI 1212 = 100 %)12%
WeldabilityNot recommended12/100
Formability (cold)Not recommended3/100
CastabilityGood60/100
Brazeability / SolderabilityPoor25/100
PolishabilityVery good75/100
Anodizing Responsen/a — copper-base alloy; use chemical passivation, oxide/patina finishes or plating instead of anodizing

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

Working with C62500-TQ50

Is C62500 easy to machine?

Machine in the as-extruded or annealed condition with rigid setups, sharp carbide tooling, positive rake, low speed (~25–45 m/min) and heavy flood coolant; chips are short and abrasive, rating ≈20% of free-cutting brass.

Can C62500 be welded?

Poor weldability — GTAW/GMAW with matching aluminium-bronze filler only where unavoidable, preheat 150–250 °C, low heat input and post-weld temper to limit brittle gamma-2 and quench cracking; not recommended for hardened parts.

Can C62500 be formed, bent or molded?

Essentially a hot-working alloy: forge/extrude at 750–870 °C; cold forming and bending should be avoided because elongation is typically ≤3%.

What surface finishes work on C62500?

Takes a bright polish and can be tin/nickel/chrome plated after thorough alumina-film removal; not anodizable — grind or hard-turn hardened parts and passivate or oil for storage.

C62500 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
Al12.5 – 13.513
Fe3.5 – 5.54.3
Mn≤ 20.5
Other (total)sum of unnamed elements≤ 0.5—
Curemainder, Cu + named elements ≥ 99.5%≥ 78.5 (balance)—

C62500-TQ50 — frequently asked

What is C62500-TQ50 used for?

C62500-TQ50 is typically used for wear-resistant parts, dies, hard-facing stock and high-load bushings. In short: hardest wrought aluminum bronze; wear and die stock; almost no ductility.

What is the yield strength of C62500-TQ50?

C62500-TQ50 has a typical yield strength of 550 MPa (79.8 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 92% of copper alloy grades. Strength varies by condition: see the 6 listed tempers.

Is C62500-TQ50 easy to machine?

Not especially — machinability is rated not recommended (14/100, worse than 100% of copper alloy grades). Machine in the as-extruded or annealed condition with rigid setups, sharp carbide tooling, positive rake, low speed (~25–45 m/min) and heavy flood coolant; chips are short and abrasive, rating ≈20% of free-cutting brass.

Can C62500-TQ50 be welded?

Not readily — weldability is rated not recommended (12/100). Poor weldability — GTAW/GMAW with matching aluminium-bronze filler only where unavoidable, preheat 150–250 °C, low heat input and post-weld temper to limit brittle gamma-2 and quench cracking; not recommended for hardened parts.

What surface finishes work on C62500-TQ50?

Takes a bright polish and can be tin/nickel/chrome plated after thorough alumina-film removal; not anodizable — grind or hard-turn hardened parts and passivate or oil for storage.

Can C62500-TQ50 be formed, bent or molded?

Essentially a hot-working alloy: forge/extrude at 750–870 °C; cold forming and bending should be avoided because elongation is typically ≤3%.

What is the maximum service temperature of C62500-TQ50?

C62500-TQ50 is rated for continuous use to about 250°C (482 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C62500-M30 and C62500-TQ50?

M30 is the default condition — standard stocked condition for C62500 rod and bar; good balance of hardness and availability, machine then use as-is. TQ50: water-quenched from the beta field to give martensitic β′ — maximum hardness for dies, forming tools and wear plates; very brittle, machine before hardening. Yield strength is 415 MPa in M30 versus 550 MPa in TQ50.

Sources

  1. ASTM B150/B150M — Aluminum Bronze Rod, Bar, and Shapes — ASTM International (2019)
  2. ASTM B601 — Temper Designations for Copper and Copper Alloys — ASTM International (2019)
  3. CDA Alloy Database — UNS C62500 — Copper Development Association (2023)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. ASM Handbook Vol. 13B — Corrosion: Materials — ASM International (2005)

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.