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Copper Alloy C72950-AT120

Precip hard

UNS C72950

AT120 = spinodally age hardened, 120 ksi min UTS

Higher-strength aged rod/bar for heavily loaded bushings and downhole components where a little ductility can be traded away.

High cost $$$$

Values for the AT120 condition

Other C72950 tempers and conditions

C72950 is listed in 4 conditions; see the grade overview at C72950.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution heat treated
Soft supersaturated condition for forming, deep drawing or machining before the customer performs spinodal ageing.32055035175 HB5 % IACS
AT110Default
Solution treated, cold worked and spinodally age hardened, 110 ksi min…
The standard stocked rod/bar condition — best balance of 760+ MPa strength, ductility and machinability for bearings and bushings.7208301232 HRC8 % IACS
AT120This page
Spinodally age hardened, 120 ksi min UTS
Higher-strength aged rod/bar for heavily loaded bushings and downhole components where a little ductility can be traded away.800900934 HRC9 % IACS
Mill hardened strip/wire, 160 ksi UTS class
Highest-strength cold-rolled plus aged strip and wire for springs, contacts and connectors; very limited formability.1,0801,150340 HRC9 % IACS

What is C72950-AT120?

C72950-AT120 is C72950 in the AT120 condition — higher-strength aged rod/bar for heavily loaded bushings and downhole components where a little ductility can be traded away. C72950-AT120 has a yield strength of 800 MPa (116 ksi) and a tensile strength of 900 MPa (131 ksi) — stronger than 98% of copper alloy grades. Elongation at break is 9% and the elastic modulus is 138 GPa (20 Msi). C72950-AT120 has a density of 8.86 g/cm³ (0.32 lb/in³), heavier than 68% of copper alloy grades. It melts at 1,040°C (1,904 °F). AT110 is the default condition FabDigit quotes; AT120 is available on request or by drawing note.

Advantages

  • High strength — 800 MPa (116 ksi), better than 98% of copper alloy grades
  • Stiff — 138 GPa (20 Msi), better than 95% of copper alloy grades
  • Easy to machine — 68/100, better than 77% of copper alloy grades
  • High service temperature — 260°C (500 °F), better than 75% of copper alloy grades

Limitations

  • Poor heat conductor — 34 W/m·K (19.6 BTU/hr·ft·°F), worse than 88% of copper alloy grades
  • High embodied carbon — 4.8 kg CO₂/kg, worse than 84% of copper alloy grades
  • Limited ductility — 9%, worse than 79% of copper alloy grades
  • Low electrical conductivity — 9 % IACS, worse than 78% of copper alloy grades

C72950-AT120 properties

Typical room-temperature values for C72950-AT120; 14 are specific to this condition. Other listed values are C72950 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C72950-AT120 has a density of 8.86 g/cm³ (0.32 lb/in³), heavier than 68% of copper alloy grades. It melts at 1,040°C (1,904 °F).

Density8.86 g/cm³0.32 lb/in³
Melting Point (Solidus)1,040°C1,904 °F
Liquidus Temperature1,130°C2,066 °F

Mechanical16

C72950-AT120 has a yield strength of 800 MPa (116 ksi) and a tensile strength of 900 MPa (131 ksi) — stronger than 98% of copper alloy grades. Elongation at break is 9% and the elastic modulus is 138 GPa (20 Msi).

Elastic (Young's) Modulus138 GPa20 Msi
Shear Modulus52 GPa7.5 Msi
Bulk Modulus128 GPa18.6 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)900 MPa131 ksi
Yield Strength (0.2% offset)800 MPa116 ksi
Elongation at Break9%
Reduction in Area20%
Compressive Strength760 MPa110 ksi
Shear Strength540 MPa78.3 ksi
Fatigue Strength (Endurance Limit)370 MPa53.7 ksi
Fracture Toughness (K_IC)45 MPa·√m41 ksi·√in
Charpy V-Notch Impact (RT)15 J11.1 ft·lbf
Hardness, Brinell320 HB
Hardness, Rockwell C34 HRC
Hardness, Vickers345 HV

Thermal6

C72950-AT120 is rated for continuous service to 260°C (500 °F). It conducts heat at 34 W/m·K (19.6 BTU/hr·ft·°F), worse than 88% of copper alloy grades. Thermal expansion is 16.5 µm/m·K (9.17 µin/in·°F).

Thermal Conductivity34 W/m·K19.6 BTU/hr·ft·°F
Specific Heat Capacity380 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.5 µm/m·K9.2 µin/in·°F
Latent Heat of Fusion200 J/g86 BTU/lb
Max Service Temperature (continuous)260°C500 °F
Min Service Temperature-200°C-328 °F

Electrical3

C72950-AT120 conducts electricity at 9 % IACS, worse than 78% of copper alloy grades.

Electrical Conductivity9 % IACS
Electrical Resistivity2.15×10⁻⁷ Ω·m8.46 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (68/100), better than 69% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.25 V
Corrosion ResistanceGood68/100
Chemical Resistance SummaryGood resistance to seawater, brine, drilling muds and sour (H2S) environments; resists sulfide stress cracking and dezincification. Attacked by oxidizing acids, ammonia/amine solutions and strong oxidizers.

Sustainability4

Producing a kilogram of C72950-AT120 takes about 68 MJ of energy and emits 4.8 kg of CO₂ — more than 83% of copper alloy grades. Typical recycled content is 20%.

Embodied Energy (primary production)68 MJ/kg29,235 BTU/lb
Embodied Carbon (primary production)4.8 kg CO₂/kg
Embodied Water260 L/kg31.2 gal/lb
Typical Recycled Content20%

Manufacturability6

C72950-AT120's machinability is good (68/100, better than 77% of copper alloy grades); weldability poor (30/100); formability poor (25/100).

MachinabilityGood68/100
Machinability Rating (AISI 1212 = 100 %)60%
WeldabilityPoor30/100
Formability (cold)Poor25/100
Brazeability / SolderabilityGood60/100
PolishabilityVery good80/100

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

Working with C72950-AT120

Is C72950 easy to machine?

Machines cleanly with short chips in the aged AT tempers — use sharp carbide, moderate speed (~120–180 m/min) and positive rake; avoid machining the gummy TX00 solution-treated state.

Can C72950 be welded?

Fusion welding is not recommended for load-bearing joints — the HAZ over-ages and loses strength; use mechanical fastening, shrink fits or brazing with re-ageing if unavoidable.

Can C72950 be formed, bent or molded?

Form, bend or draw only in the TX00 solution-treated temper and age afterwards; aged AT/TS tempers tolerate little cold bending.

What surface finishes work on C72950?

Polishes to a bright bronze finish and accepts electroless nickel, silver or tin plating; no anodizing (copper alloy) — light oxidation gives a natural protective film.

C72950 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
Nispinodal-forming solute14.5 – 15.515
Sn7.5 – 8.58
Fe≤ 0.5—
Mn≤ 0.3—
Zn≤ 0.5—
Nbgrain-refining addition, when present≤ 0.3—
Pb≤ 0.02—
Cubalance, ~76 %balance—

C72950-AT120 — frequently asked

What is C72950-AT120 used for?

C72950-AT120 is typically used for heavy-duty bearings, bushings, connectors and landing gear components. In short: strongest spinodal copper-nickel; beryllium-copper replacement; high-load bearing bronze.

What is the yield strength of C72950-AT120?

C72950-AT120 has a typical yield strength of 800 MPa (116 ksi) and a tensile strength of 900 MPa (131 ksi) — stronger than 98% of copper alloy grades. Strength varies by condition: see the 4 listed tempers.

Is C72950-AT120 easy to machine?

Reasonably — machinability is rated good (68/100, better than 77% of copper alloy grades). Machines cleanly with short chips in the aged AT tempers — use sharp carbide, moderate speed (~120–180 m/min) and positive rake; avoid machining the gummy TX00 solution-treated state.

Can C72950-AT120 be welded?

Not readily — weldability is rated poor (30/100). Fusion welding is not recommended for load-bearing joints — the HAZ over-ages and loses strength; use mechanical fastening, shrink fits or brazing with re-ageing if unavoidable.

What surface finishes work on C72950-AT120?

Polishes to a bright bronze finish and accepts electroless nickel, silver or tin plating; no anodizing (copper alloy) — light oxidation gives a natural protective film.

Can C72950-AT120 be formed, bent or molded?

Form, bend or draw only in the TX00 solution-treated temper and age afterwards; aged AT/TS tempers tolerate little cold bending.

What is the maximum service temperature of C72950-AT120?

C72950-AT120 is rated for continuous use to about 260°C (500 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C72950-AT110 and C72950-TX00?

AT110 is the default condition — the standard stocked rod/bar condition — best balance of 760+ MPa strength, ductility and machinability for bearings and bushings. TX00: soft supersaturated condition for forming, deep drawing or machining before the customer performs spinodal ageing. Yield strength is 720 MPa in AT110 versus 320 MPa in TX00.

Sources

  1. ToughMet 3 AT / TS Alloy Data Sheets — Materion Brush Performance Alloys (2022)
  2. ASTM B929 — Standard Specification for Wrought Copper-Nickel-Tin Spinodal Alloy Rod, Bar and Wire — ASTM International (2021)
  3. CDA Alloy Database — C72900/C72950 Cu-Ni-Sn spinodal alloys — Copper Development Association (2023)
  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.