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Copper Alloy C96900 TX00-HS

Precip hard

UNS C96900 · EN CC383H, CuNi30Fe1Mn1NbSi-C

TX00-HS = tX00 high-strength age

Peak-aged producer temper for the highest yield and galling resistance in downhole and heavily loaded subsea bearings; accept lower elongation and impact.

High cost $$$$

Values for the TX00-HS condition

Other C96900 tempers and conditions

C96900 is listed in 5 conditions; see the grade overview at C96900.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
As sand cast
Soft as-cast sand castings, ordered when the part will be spinodally aged after rough machining or when maximum ductility is wanted.24048012160 HB7 % IACS
As centrifugally cast
Centrifugally cast sleeves/rings in the unhardened condition, normally a semi-finished stage before TX00 aging.26052015170 HB7 % IACS
As continuous cast
Continuous-cast bar/tube stock in the soft condition — the usual purchase form for shops that heat treat in-house.27555018180 HB7.5 % IACS
TX00Default
Spinodal heat treated
Standard commercial hardened condition — best balance of ~650 MPa yield, wear/galling resistance and residual ductility for bearings, bushings and valve parts.655795828 HRC11 % IACS
TX00-HSThis page
TX00 high-strength age
Peak-aged producer temper for the highest yield and galling resistance in downhole and heavily loaded subsea bearings; accept lower elongation and impact.745860532 HRC12 % IACS

What is C96900 TX00-HS?

C96900 TX00-HS is C96900 in the TX00-HS condition — peak-aged producer temper for the highest yield and galling resistance in downhole and heavily loaded subsea bearings; accept lower elongation and impact. C96900 TX00-HS has a yield strength of 745 MPa (108 ksi) and a tensile strength of 860 MPa (125 ksi) — stronger than 97% of copper alloy grades. Elongation at break is 5% and the elastic modulus is 138 GPa (20 Msi). C96900 TX00-HS has a density of 8.94 g/cm³ (0.323 lb/in³), heavier than 90% of copper alloy grades. It melts at 1,010°C (1,850 °F). TX00 is the default condition FabDigit quotes; TX00-HS is available on request or by drawing note.

Advantages

  • High strength — 745 MPa (108 ksi), better than 97% of copper alloy grades
  • Stiff — 138 GPa (20 Msi), better than 95% of copper alloy grades
  • Good corrosion resistance — 78/100, better than 94% of copper alloy grades

Limitations

  • High embodied carbon — 6.5 kg CO₂/kg, worse than 94% of copper alloy grades
  • Limited ductility — 5%, worse than 93% of copper alloy grades
  • Poor heat conductor — 42 W/m·K (24.3 BTU/hr·ft·°F), worse than 80% of copper alloy grades
  • Limited formability — 15/100, worse than 79% of copper alloy grades
  • Difficult to weld — 25/100, worse than 78% of copper alloy grades

C96900 TX00-HS properties

Typical room-temperature values for C96900 TX00-HS; 12 are specific to this condition. Other listed values are C96900 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C96900 TX00-HS has a density of 8.94 g/cm³ (0.323 lb/in³), heavier than 90% of copper alloy grades. It melts at 1,010°C (1,850 °F).

Density8.94 g/cm³0.32 lb/in³
Melting Point (Solidus)1,010°C1,850 °F
Liquidus Temperature1,120°C2,048 °F

Mechanical15

C96900 TX00-HS has a yield strength of 745 MPa (108 ksi) and a tensile strength of 860 MPa (125 ksi) — stronger than 97% of copper alloy grades. Elongation at break is 5% 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)860 MPa125 ksi
Yield Strength (0.2% offset)745 MPa108 ksi
Elongation at Break5%
Reduction in Area12%
Compressive Strength700 MPa102 ksi
Shear Strength480 MPa69.6 ksi
Fatigue Strength (Endurance Limit)260 MPa37.7 ksi
Charpy V-Notch Impact (RT)10 J7.4 ft·lbf
Hardness, Brinell300 HB
Hardness, Rockwell C32 HRC
Hardness, Vickers320 HV

Thermal5

C96900 TX00-HS is rated for continuous service to 250°C (482 °F). It conducts heat at 42 W/m·K (24.3 BTU/hr·ft·°F), worse than 80% of copper alloy grades. Thermal expansion is 16.4 µm/m·K (9.11 µin/in·°F).

Thermal Conductivity42 W/m·K24.3 BTU/hr·ft·°F
Specific Heat Capacity380 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.4 µm/m·K9.1 µin/in·°F
Max Service Temperature (continuous)250°C482 °F
Min Service Temperature-196°C-321 °F

Electrical3

C96900 TX00-HS conducts electricity at 12 % IACS, worse than 62% of copper alloy grades.

Electrical Conductivity12 % IACS
Electrical Resistivity1.57×10⁻⁷ Ω·m6.18 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (78/100), better than 94% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.26 V
Corrosion ResistanceVery good78/100
Chemical Resistance SummaryVery good in seawater, brines, drilling muds and sour (H2S/CO2) environments; resists stress-corrosion cracking in ammonia and chloride service better than brasses/aluminium bronzes; attacked by oxidising acids (nitric), strong ammonia liquors and sulphur-bearing molten media.

Sustainability4

Producing a kilogram of C96900 TX00-HS 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 Water400 L/kg47.9 gal/lb
Typical Recycled Content30%

Manufacturability8

C96900 TX00-HS's machinability is good (55/100, better than 71% of copper alloy grades); weldability poor (25/100); formability poor (15/100).

MachinabilityGood55/100
Machinability Rating (AISI 1212 = 100 %)40%
WeldabilityPoor25/100
Formability (cold)Poor15/100
CastabilityGood62/100
Brazeability / SolderabilityFair45/100
PolishabilityVery good80/100
Anodizing Responsen/a — copper alloy; use passivation, tin/silver plate or phosphating instead

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

Working with C96900 TX00-HS

Is C96900 easy to machine?

Machines well in the aged TX00 temper with sharp carbide tooling, positive rake and modest speeds (60–120 m/min); chips break cleanly, no lead needed, and the soft as-cast temper is gummier than the hardened one.

Can C96900 be welded?

Not recommended for structural joints — fusion welding over-ages the spinodal structure and risks tin segregation cracking; use mechanical joints, or requalify with a full post-weld solution + aging cycle.

Can C96900 be formed, bent or molded?

Supplied as continuous, centrifugal or sand castings; control pour temperature and cooling to avoid tin inverse segregation, and rough-machine before the spinodal age for best dimensional stability.

What surface finishes work on C96900?

Takes a fine bearing-grade polish (Ra < 0.4 µm); tin, silver or chemical Ni plating is possible for anti-galling or electrical contact duty — anodizing does not apply.

C96900 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
NiNi + Co may be reported together14.5 – 15.515
Snspinodal hardening element7.5 – 8.58
Fe≤ 0.50.15
Zn≤ 0.50.1
Mndeoxidiser≤ 0.30.1
Nbgrain refiner, optional≤ 0.1—
Pbkeep low for hot-tear resistance≤ 0.02—
Curemainder, nominally ~76.5 %balance—

C96900 TX00-HS — frequently asked

What is C96900 TX00-HS used for?

C96900 TX00-HS is typically used for large ship propellers, high-load marine pump castings and offshore structural fittings. In short: strongest cast Cu-Ni; nb-microalloyed propeller grade; higher strength than C96400.

What is the yield strength of C96900 TX00-HS?

C96900 TX00-HS has a typical yield strength of 745 MPa (108 ksi) and a tensile strength of 860 MPa (125 ksi) — stronger than 97% of copper alloy grades. Strength varies by condition: see the 5 listed tempers.

Is C96900 TX00-HS easy to machine?

Reasonably — machinability is rated good (55/100, better than 71% of copper alloy grades). Machines well in the aged TX00 temper with sharp carbide tooling, positive rake and modest speeds (60–120 m/min); chips break cleanly, no lead needed, and the soft as-cast temper is gummier than the hardened one.

Can C96900 TX00-HS be welded?

Not readily — weldability is rated poor (25/100). Not recommended for structural joints — fusion welding over-ages the spinodal structure and risks tin segregation cracking; use mechanical joints, or requalify with a full post-weld solution + aging cycle.

What surface finishes work on C96900 TX00-HS?

Takes a fine bearing-grade polish (Ra < 0.4 µm); tin, silver or chemical Ni plating is possible for anti-galling or electrical contact duty — anodizing does not apply.

Can C96900 TX00-HS be formed, bent or molded?

Supplied as continuous, centrifugal or sand castings; control pour temperature and cooling to avoid tin inverse segregation, and rough-machine before the spinodal age for best dimensional stability.

What is the maximum service temperature of C96900 TX00-HS?

C96900 TX00-HS 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 C96900-TX00 and C96900-M01?

TX00 is the default condition — standard commercial hardened condition — best balance of ~650 MPa yield, wear/galling resistance and residual ductility for bearings, bushings and valve parts. M01: soft as-cast sand castings, ordered when the part will be spinodally aged after rough machining or when maximum ductility is wanted. Yield strength is 655 MPa in TX00 versus 240 MPa in M01.

Sources

  1. ASTM B505/B505M — Continuous Cast Copper Alloy Castings — ASTM International (2018)
  2. ASTM B929 — Copper-Nickel-Tin Spinodal Alloy Castings — ASTM International (2020)
  3. ASTM B601 — Temper Designations for Copper and Copper Alloys — ASTM International (2019)
  4. ToughMet 3 CX (UNS C96900) cast alloy datasheet — Materion Brush Performance Alloys (2021)
  5. UNS C96900 alloy record / Copper Alloy Data — Copper Development Association (copper.org) (2023)
  6. 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.