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Material Specification

Copper Nickel C72900

Copper Nickel C72900 Fasteners
Cu-15Ni-8Sn Spinodal — Up to 1138 MPa

Copper Nickel C72900 Fasteners

Copper Nickel C72900 is the Cu-15Ni-8Sn spinodal alloy, and it is a different material from everything else on this hub. Nickel is 14.5–15.5% with 7.5–8.5% tin, plus small magnesium, manganese and niobium additions, and copper plus named elements at 99.7% minimum. It is covered by its own standards — ASTM B929 for rod and bar and ASTM B740 for strip — which describe it as a copper-nickel-tin spinodal alloy.

Spinodal decomposition is not precipitation hardening. Rather than forming discrete second-phase particles, the alloy separates on ageing into finely interleaved tin-rich and tin-poor regions on a nanometre scale, with no distinct particle boundary. That structure obstructs dislocation movement extremely effectively, and the results are remarkable for a copper alloy: ASTM minimums of 1138 MPa tensile with 1000 MPa yield at the TS04 hard-and-spinodal-hardened temper. C72900 is a genuine high-strength structural and bearing material — the alloy behind heavy-duty bushings and bearings in oilfield, aerospace and marine service — and is non-magnetic and non-sparking with it. Exotic Alloy supplies C72900 to ASTM B929 and B740.

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Product Range

Copper Nickel C72900 Fasteners Available

Copper Nickel C72900 Hex Bolts
Copper Nickel C72900
Hex Bolts
Copper Nickel C72900 Heavy Hex Bolts
Copper Nickel C72900
Heavy Hex Bolts
Copper Nickel C72900 Stud Bolts
Copper Nickel C72900
Stud Bolts
Copper Nickel C72900 Threaded Rods
Copper Nickel C72900
Threaded Rods
Copper Nickel C72900 Anchor Bolts
Copper Nickel C72900
Anchor Bolts
Copper Nickel C72900 Hex Nuts
Copper Nickel C72900
Hex Nuts
Copper Nickel C72900 Washers
Copper Nickel C72900
Washers
Copper Nickel C72900 Cotter Pins
Copper Nickel C72900
Cotter Pins
Copper Nickel C72900 Springs
Copper Nickel C72900
Springs
Copper Nickel C72900 Circlips
Copper Nickel C72900
Circlips
Copper Nickel C72900 Coated Fasteners
Copper Nickel C72900
Coated Fasteners
Copper Nickel C72900 Custom Spacers
Copper Nickel C72900
Custom Spacers
Technical Data

Copper Nickel C72900 Specifications

Chemical Composition — Copper Nickel C72900 (wt. %)
ElementMinimum %Maximum %
Copper (Cu), including silverRemainder—
Nickel (Ni), including cobalt14.515.5
Tin (Sn)7.58.5
Zinc (Zn)—0.50
Iron (Fe)—0.50
Manganese (Mn)—0.30
Magnesium (Mg)—0.15
Niobium (Nb)—0.10
Lead (Pb)—0.02*
Copper + sum of named elements99.7—
Mechanical Properties — Copper Nickel C72900
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
Solution heat treated TB00 (min)44116532—
Sol. treated + 1/4 hard TD01 (min)51734518—
Sol. treated + 1/2 hard TD02 (min)586—8—
Sol. treated + 3/4 hard TD03 (min)6555523—
Sol. treated + hard TD04 (min)689586——
Spinodal hardened, low strength TX00 (min)8276556—
Mill hardened TM00 (min)65551722—
Mill hardened 1/2 hard TM02 (min)72462115—
Mill hardened hard TM04 (min)79372410—
Mill hardened extra hard TM06 (min)8968276—
Mill hardened spring TM08 (min)10349652—
1/4 hard + spinodal hardened TS01 (min)8967244—
1/2 hard + spinodal hardened TS02 (min)10008623—
3/4 hard + spinodal hardened TS03 (min)10699312—
Hard + spinodal hardened TS04 (min)113810002—
Physical Properties
Density8.94 g/cm³ (0.323 lb/in³)
Melting Point — Liquidus1115 °C (2039 °F)
Melting Point — Solidus950 °C (1742 °F)
Electrical Conductivity7.8% IACS at 20 °C, aged
Thermal Conductivity29 W/m·K at 20 °C
Coefficient of Thermal Expansion16.4 × 10⁻⁶ /°C (20–300 °C)
Specific Heat Capacity377 J/kg·K at 20 °C
Modulus of Elasticity128 GPa
Modulus of Rigidity52 GPa
Annealing Temperature824 °C (1515 °F)
Hot Working Temperature649–871 °C (1200–1600 °F)
Strengthening MechanismSpinodal decomposition — not precipitation
Magnetic ResponseNon-magnetic; non-sparking
Equivalent Grades & Standards
UNSEN / CEN DesignationNominal CompositionCommon Name
C72900 — Cu-15Ni-8Sn (spinodal) Copper-Nickel-Tin Spinodal Alloy

Key Specifications: ASTM B929 (Copper-Nickel-Tin Spinodal Alloy Rod and Bar) / ASTM B740 (Copper-Nickel-Tin Spinodal Alloy Strip).

*Lead is limited to 0.005% maximum for hot rolling.

C72900 has its own dedicated ASTM standards rather than sitting under the general copper-nickel specifications, which reflects how different a material it is. It is not covered by ASTM B466 or by ASTM F468.

Note on fastener standards: Of the alloys on this hub, only C71500 is covered by the ASTM nonferrous fastener standards. ASTM F468 and F467 list C71500 (as Cu 715) along with C71000 and a range of brasses and bronzes — but C70600 is not among them, and neither are the other grades here. That is a genuinely useful distinction: where a certified copper-nickel bolt, hex cap screw, stud or nut is required, C71500 (70/30) is the grade that has a standard behind it, and specifying 90/10 instead means the fastener is supplied to the mill product requirements with acceptance criteria agreed on the order rather than to a fastener specification.

On strength, annealed 70/30 is specified at 345 MPa minimum and hard-drawn at 485 MPa, against 830 MPa for an ordinary ASTM A325 structural steel bolt. Copper-nickel fasteners are chosen for seawater corrosion resistance, biofouling resistance, freedom from chloride stress-corrosion cracking and compatibility with copper-nickel pipework — not for load. The one exception on this hub is C72900, the spinodal Cu-15Ni-8Sn alloy, which reaches 1138 MPa and is a genuine high-strength material.

Every copper-nickel order ships with EN 10204 3.1 certification giving the heat analysis, the temper, and the mechanical test results for the product form and section supplied. Iron and manganese are reported explicitly on the 90/10 and 70/30 grades, because iron within the specified range is what makes the protective seawater film work and material at the bottom of the range performs measurably worse. Carbon, phosphorus and sulfur are reported on the welding grades C70620 and C71520, where they are the whole reason for the grade. Positive material identification, hardness testing and additional NDT can be added at order stage.

Machining: the copper-nickels carry a CDA machinability rating of 20, the same as pure copper, where free-cutting brass C36000 is 100. They are tough and gummy, they work harden ahead of the tool, and they produce long continuous swarf with a strong tendency to build up on the cutting edge. Sharp positive-rake tooling kept genuinely sharp, rigid setups, a positive feed that keeps the tool cutting rather than rubbing, moderate speeds and generous lubricant are all needed. Dwelling or allowing the tool to rub will work-harden the surface and ruin the next pass.

Forming: capacity for cold working and hot forming are both rated Good. Copper-nickels bend, draw, spin and cold head satisfactorily, though they work harden faster than pure copper and interstage annealing is needed for severe work. Threads are rolled rather than cut wherever section permits.

Welding is a real strength of this family, and it is unusual among copper alloys. CDA rate C71500 Excellent for soldering, brazing, gas-shielded arc welding, coated metal arc welding, spot, seam and butt welding — a clean sweep that no pure copper comes close to, because the nickel reduces thermal conductivity enough that the weld pool can actually be established. C70600 is nearly as good, rated Excellent for soldering, brazing, gas-shielded arc and butt welding and Good for coated metal arc, spot and seam welding. Two cautions apply: avoid oxyacetylene welding where possible, and keep the weld bore free of penetration and spatter, because a protruding root bead in a seawater line creates exactly the local turbulence that initiates impingement attack.

C72900 specifically: CDA rate the alloy Excellent for soldering, brazing, gas-shielded arc, coated metal arc, spot, seam and butt welding, and Excellent for cold working — a notably better joining profile than the pure coppers. Machining is normally done in the solution-treated or cold-worked condition before spinodal hardening, since the fully hardened material at over 1000 MPa is considerably harder on tooling. The alloy is non-sparking, which matters for the oilfield and hazardous-area bearing applications it is commonly specified for.

Heat treatment: C72900 is strengthened by spinodal decomposition, which is a distinct mechanism from the precipitation hardening used in chromium copper and worth understanding. On ageing, the solid solution separates continuously into nanometre-scale tin-rich and tin-poor regions without forming discrete particles or distinct phase boundaries. Because there is no nucleation step, the structure develops uniformly throughout the section — which means, unlike a precipitation-hardening alloy, heavy sections do not suffer the property fall-off that quench rate imposes.

The processing route is solution treatment, optional cold work, then the spinodal ageing treatment. CDA give an annealing temperature of 824 °C (1515 °F) and hot working at 649–871 °C. The temper designations record the route: TB00 solution treated; TD01–TD04 solution treated and cold worked; TS01–TS04 cold worked and then spinodal hardened, giving the highest properties; TM00–TM08 mill-hardened tempers supplied ready to use; and TX00 a lower-strength spinodal condition. Specify the temper explicitly — the range runs from 441 to 1138 MPa.

C72900 is the high-strength outlier of the copper-nickel family. At up to 1138 MPa it is roughly three times the strength of annealed 70/30 and comparable with a heat-treated alloy steel, while remaining non-magnetic and non-sparking — the combination that makes it the standard choice for heavy-duty bushings and bearings in oilfield drilling equipment, aerospace landing gear and marine shafting. Its resistance to galling and its bearing behaviour under high load are as important commercially as its tensile strength.

On corrosion, CDA publish no corrosion data for C72900 and the alloy is not a direct substitute for the marine grades: it carries no deliberate iron addition and has not been characterised in flowing seawater the way C70600 and C71500 have. Where it is used in marine service it is generally as a mechanical component rather than as pressure boundary or heat-transfer surface. The electrical conductivity of 7.8% IACS in the aged condition confirms it is a structural material, not a conductor.

Seawater is what copper-nickels are for, and they are the benchmark against which other marine alloys are judged. The 90/10 and 70/30 grades combine good general corrosion resistance in salt water with two properties that very few other materials offer together: high resistance to chloride stress-corrosion cracking, which is the mechanism that limits austenitic stainless steel in warm seawater, and inherent resistance to macrofouling. The copper ion released at the surface deters barnacle, mussel and algal settlement, so copper-nickel seawater piping, condenser tubing, sheathing and intake screens stay substantially cleaner than stainless or titanium equivalents without chlorination or antifouling coatings. For a heat exchanger that is a thermal performance advantage as well as a maintenance one.

The iron content is deliberate and it is what makes the protective film work. The 1.0–1.8% iron in C70600 and the 0.40–1.0% in C71500 are not impurities — iron is essential to forming the adherent, protective cuprous oxide film that gives these alloys their impingement resistance. Material at the bottom of the iron range, or with the iron tied up as coarse precipitate rather than in solution, performs measurably worse. This is a reason to buy certified material and to read the heat analysis rather than assume.

Copper-nickels have a velocity ceiling, and exceeding it is the most common way they are misapplied. Above a critical flow velocity the protective film is stripped faster than it can reform and the alloy suffers erosion-corrosion — impingement attack, typically showing as horseshoe-shaped pits pointing downstream. The commonly applied design limits are roughly 3.0–3.5 m/s for 90/10 (C70600) and 4.0–4.5 m/s for 70/30 (C71500), with the higher nickel content buying the extra margin. Those are design figures for clean seawater in well-made pipework, and local velocity matters more than bulk velocity: partly closed valves, sharp bends, badly made joints with weld penetration into the bore, and entrained air or sand all create local conditions far worse than the nominal flow. Where velocity genuinely cannot be held down, 70/30 rather than 90/10, or a different alloy family, is the answer.

Two service conditions attack copper-nickels, and both are avoidable by operating practice. The first is sulfide-polluted seawater. Hydrogen sulfide and other sulfides — from stagnant harbour water, anaerobic mud, decaying organic matter or polluted estuarine water — interfere with formation of the protective film and produce a black, non-protective corrosion product in its place. Attack can be rapid, and material that has been exposed to sulfides before its protective film matured may never develop proper resistance.

The second is stagnation, which is in practice the commissioning problem. A new copper-nickel seawater system needs time with clean, flowing, aerated seawater to develop its protective film — a matter of weeks to months for full maturity. A system that is hydrotested with seawater and then left full and stagnant during fit-out is the classic failure case: the water goes anaerobic, sulfides form, and the film never establishes properly. The established practice is to commission with clean seawater at design flow, or to drain and dry completely between tests, and never to leave the system wet and still.

Copper-nickels are markedly more resistant to stress-corrosion cracking than the brasses, which is one of their quiet advantages. Dezincification does not apply — there is no zinc to lose — and the ammonia stress-corrosion cracking that destroys brass fittings is far less of a threat here. They are also resistant to the chloride SCC that limits austenitic stainless steel in warm seawater, which is the reason copper-nickel rather than 316 is specified for many seawater services. That said, the alloys are not immune: concentrated ammonia and amine environments should still be treated with caution for stressed components such as tightened fasteners, and stress relief after heavy cold work remains sensible practice for parts going into borderline service.

Galvanically the copper-nickels sit usefully in the middle of the seawater series. They are more noble than carbon steel, cast iron, aluminium and zinc, so a copper-nickel fastener will drive corrosion of those materials and needs isolation from them — the classic problem being copper-nickel pipework bolted into a steel structure. They are less noble than the passive stainless steels, titanium and the high-molybdenum nickel alloys, so in a mixed seawater system with those materials the copper-nickel is the part that suffers, and the area ratio matters: a small copper-nickel component among large titanium surfaces is the bad case. They are compatible with the other coppers and bronzes and with Monel. Copper-nickel is also commonly used as the sacrificial partner in controlled fashion — coupling to a small area of steel is sometimes deliberate.

C70620 and C71520 exist specifically for welded fabrication, and ASME SB-466 says so outright: the standard states that these two alloys “are intended for product that will be subsequently welded.” They are the same nominal 90/10 and 70/30 compositions as C70600 and C71500 but with three elements tightened sharply: carbon to 0.05%, phosphorus to 0.02% and sulfur to 0.02%, where the standard grades carry no limit on carbon or sulfur at all. Those three are the elements that cause porosity and hot cracking in a copper-nickel weld, and controlling them is the difference between a sound weld and a leaking one. Specify the welding grade whenever the component will be welded in fabrication — the mechanical requirements under SB-466 are identical, so there is no property penalty for doing so.

How these grades divide. The two that matter for most marine work are C70600 (90/10) and C71500 (70/30). The 70/30 is stronger — 345 MPa against 262 MPa annealed — tolerates a higher flow velocity, performs better hot, and is the one carried by ASTM F468 for fasteners; the 90/10 is cheaper, conducts heat better at 45 against 29 W/m·K, and is adequate for the majority of seawater service. C70620 and C71520 are the same two compositions with carbon, phosphorus and sulfur tightened for welded fabrication. C71580 is a 70/30 variant with iron and manganese cut right back. Beyond those, the family diverges sharply: C72150 at 43–46% nickel is a Constantan-type electrical resistance alloy, not a marine material; C72420 adds aluminium and manganese for higher strength; and C72900 is a spinodally hardened Cu-15Ni-8Sn alloy reaching 1138 MPa, a different material in everything but name. Alloy 130 and Alloy 191 sit outside the copper-nickel class altogether — see the notes on those pages.

Key Characteristics

  • Cu-15Ni-8Sn spinodal alloy — up to 1138 MPa tensile.
  • Strengthened by spinodal decomposition, not precipitation.
  • No nucleation step — heavy sections do not suffer quench-rate fall-off.
  • Fifteen specified tempers from 441 MPa (TB00) to 1138 MPa (TS04).
  • Own ASTM standards: B929 for rod and bar, B740 for strip.
  • Non-magnetic and non-sparking.
  • Excellent bearing and anti-galling behaviour under high load.
  • Rated Excellent by CDA for every joining process listed.

Typical Applications

  • Heavy-duty bushings and bearings for oilfield drilling equipment.
  • Aerospace landing gear bushings and bearing components.
  • Marine shafting, bearings and high-load mechanical hardware.
  • High-strength non-magnetic fasteners and fixings.
  • Downhole tool components and measurement-while-drilling hardware.
  • Non-sparking tools and hazardous-area components.
  • Connectors and spring contacts in strip form.
  • Heavily loaded wear components requiring anti-galling behaviour.