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Copper Alloy C82800-M01

Finish state

UNS C82800 · ASTM B824

M01 = as sand cast

As-cast C82800 (Cu-2.6Be-Co-Si) with partially precipitated beryllium: strong and hard straight from the mould but brittle, and normally solution treated plus aged before service.

High cost $$$$

Values for the M01 condition

Other C82800 tempers and conditions

C82800 is listed in 4 conditions; see the grade overview at C82800.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution heat treated
Softest, most ductile condition — used for rough machining, straightening or repair welding before precipitation aging.24052012155 HB14 % IACS
Thermomechanically controlled processed
Raw casting condition — moderate strength, used only as a starting point before solution/aging or for low-stress parts.3105521200 HB17 % IACS
M01This page
As sand cast
As-cast C82800 (Cu-2.6Be-Co-Si) with partially precipitated beryllium: strong and hard straight from the mould but brittle, and normally solution treated plus aged before service.3105521200 HB16 % IACS
TF00Default
Solution heat treated and precipitation hardened
Standard supply condition for tooling: maximum hardness (~43 HRC) and >1000 MPa strength with useful thermal conductivity.1,0001,0690.543 HRC20 % IACS

What is C82800-M01?

C82800-M01 is C82800 supplied in the M01 condition — as-cast C82800 (Cu-2.6Be-Co-Si) with partially precipitated beryllium: strong and hard straight from the mould but brittle, and normally solution treated plus aged before service. C82800-M01 has a yield strength of 310 MPa (45 ksi) and a tensile strength of 552 MPa (80.1 ksi) — stronger than 64% of copper alloy grades. Elongation at break is 1% and the elastic modulus is 131 GPa (19 Msi). C82800-M01 has a density of 8.25 g/cm³ (0.298 lb/in³), lighter than 84% of copper alloy grades. It melts at 857°C (1,575 °F). TF00 is the default condition FabDigit quotes; M01 is available on request or by drawing note.

Advantages

  • Stiff — 131 GPa (19 Msi), better than 91% of copper alloy grades

Limitations

  • Limited ductility — 1%, worse than 99% of copper alloy grades
  • Limited formability — 5/100, worse than 98% of copper alloy grades
  • Low fracture toughness — 20 MPa·√m (18.2 ksi·√in), worse than 97% of copper alloy grades
  • High embodied carbon — 6 kg CO₂/kg, worse than 92% of copper alloy grades
  • Difficult to machine — 25/100, worse than 86% of copper alloy grades

C82800-M01 properties

Typical room-temperature values for C82800-M01; 37 are specific to this condition. Other listed values are C82800 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C82800-M01 has a density of 8.25 g/cm³ (0.298 lb/in³), lighter than 84% of copper alloy grades. It melts at 857°C (1,575 °F).

Density8.25 g/cm³0.3 lb/in³
Melting Point (Solidus)857°C1,575 °F
Liquidus Temperature954°C1,749 °F

Mechanical15

C82800-M01 has a yield strength of 310 MPa (45 ksi) and a tensile strength of 552 MPa (80.1 ksi) — stronger than 64% of copper alloy grades. Elongation at break is 1% and the elastic modulus is 131 GPa (19 Msi).

Elastic (Young's) Modulus131 GPa19 Msi
Shear Modulus50 GPa7.3 Msi
Bulk Modulus110 GPa16 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)552 MPa80.1 ksi
Yield Strength (0.2% offset)310 MPa45 ksi
Elongation at Break1%
Compressive Strength1,300 MPa189 ksi
Shear Strength370 MPa53.7 ksi
Fatigue Strength (Endurance Limit)170 MPa24.7 ksi
Fracture Toughness (K_IC)20 MPa·√m18.2 ksi·√in
Charpy V-Notch Impact (RT)3 J2.2 ft·lbf
Hardness, Brinell200 HB
Hardness, Rockwell C43 HRC
Hardness, Vickers210 HV

Thermal6

C82800-M01 is rated for continuous service to 200°C (392 °F). It conducts heat at 90 W/m·K (52 BTU/hr·ft·°F), better than 54% of copper alloy grades. Thermal expansion is 17 µm/m·K (9.44 µin/in·°F).

Thermal Conductivity90 W/m·K52 BTU/hr·ft·°F
Specific Heat Capacity419 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)17 µm/m·K9.4 µin/in·°F
Latent Heat of Fusion205 J/g88.1 BTU/lb
Max Service Temperature (continuous)200°C392 °F
Min Service Temperature-200°C-328 °F

Electrical3

C82800-M01 conducts electricity at 16 % IACS, worse than 52% of copper alloy grades.

Electrical Conductivity16 % IACS
Electrical Resistivity1.08×10⁻⁷ Ω·m4.25 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (65/100), better than 58% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.28 V
Corrosion ResistanceGood65/100
Chemical Resistance SummaryGood resistance to seawater, non-oxidising acids and industrial atmospheres; attacked by ammonia, oxidising acids and sulphides.

Sustainability4

Producing a kilogram of C82800-M01 takes about 85 MJ of energy and emits 6 kg of CO₂ — more than 92% of copper alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)85 MJ/kg36,543 BTU/lb
Embodied Carbon (primary production)6 kg CO₂/kg
Embodied Water350 L/kg41.9 gal/lb
Typical Recycled Content30%

Manufacturability8

C82800-M01's machinability is poor (25/100, worse than 86% of copper alloy grades); weldability fair (40/100); formability not recommended (5/100).

MachinabilityPoor25/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityFair40/100
Formability (cold)Not recommended5/100
CastabilityVery good80/100
Brazeability / SolderabilityGood60/100
PolishabilityVery good80/100
Anodizing Responsen/a — copper alloy; use plating (Ni/Cr) or passivation instead of anodizing

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

Working with C82800-M01

Is C82800 easy to machine?

Machinability ~20 % of AISI 1212; use sharp carbide tooling, rigid setups and flood coolant with HEPA/wet dust control — beryllium-bearing dust and fines are a health hazard.

Can C82800 be welded?

GTAW/GMAW with matching BeCu filler is possible but the weld and HAZ must be re-solutionized and re-aged; forced ventilation and fume extraction are mandatory.

Can C82800 be formed, bent or molded?

Shaped by sand, permanent-mold or investment casting only; the aged material has <1 % elongation and cannot be cold formed — do all machining before final aging where possible.

What surface finishes work on C82800?

Takes a high mold polish; commonly electroless-nickel or hard-chrome plated for corrosion/wear, and can be passivated — not anodizable.

C82800 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
Be2.5 – 2.752.6
CoCo, or Co+Ni ≥ 0.350.35 – 0.650.5
Si0.2 – 0.350.28
Nicounted with Co≤ 0.3—
FeCo+Ni+Fe ≤ 0.70≤ 0.25—
Al≤ 0.15—
Pb≤ 0.02—
Curemainder, ≈95.5 %balance—

C82800-M01 — frequently asked

What is C82800-M01 used for?

C82800-M01 is typically used for high-load mold components, non-sparking safety tools and heavy-duty bearing castings. In short: highest-strength cast BeCu; maximum hardness, minimum ductility; non-sparking safety tooling.

What is the yield strength of C82800-M01?

C82800-M01 has a typical yield strength of 310 MPa (45 ksi) and a tensile strength of 552 MPa (80.1 ksi) — stronger than 64% of copper alloy grades. Strength varies by condition: see the 4 listed tempers.

Is C82800-M01 easy to machine?

Not especially — machinability is rated poor (25/100, worse than 86% of copper alloy grades). Machinability ~20 % of AISI 1212; use sharp carbide tooling, rigid setups and flood coolant with HEPA/wet dust control — beryllium-bearing dust and fines are a health hazard.

Can C82800-M01 be welded?

With care — weldability is rated fair (40/100). GTAW/GMAW with matching BeCu filler is possible but the weld and HAZ must be re-solutionized and re-aged; forced ventilation and fume extraction are mandatory.

What surface finishes work on C82800-M01?

Takes a high mold polish; commonly electroless-nickel or hard-chrome plated for corrosion/wear, and can be passivated — not anodizable.

Can C82800-M01 be formed, bent or molded?

Shaped by sand, permanent-mold or investment casting only; the aged material has <1 % elongation and cannot be cold formed — do all machining before final aging where possible.

What is the maximum service temperature of C82800-M01?

C82800-M01 is rated for continuous use to about 200°C (392 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C82800-TF00 and C82800-TB00?

TF00 is the default condition — standard supply condition for tooling: maximum hardness (~43 HRC) and >1000 MPa strength with useful thermal conductivity. TB00: softest, most ductile condition — used for rough machining, straightening or repair welding before precipitation aging. Yield strength is 1,000 MPa in TF00 versus 240 MPa in TB00.

Sources

  1. ASTM B824 — Standard Specification for General Requirements for Copper Alloy Castings — ASTM International (2022)
  2. ASTM B770 — Copper-Beryllium Alloy Sand Castings for General Applications — ASTM International (2019)
  3. CDA/UNS C82800 Alloy Datasheet — Copper Development Association (copper.org) (2023)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. Cast Beryllium Copper Alloys — Technical Data — Materion Brush Performance Alloys (2022)

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.