Copper Alloys dealers in UAE

C17200 / CuBe2 / CW101C

C17200 / CuBe2 (2.1247, CW101C) - the highest-strength commercially available copper alloy. UTS up to 1400 MPa HT condition. Available per AMS 4534, AMS 4533, and MIL-C-21657 for aerospace and defence applications. Note: beryllium-containing alloy - observe all applicable health and safety regulations.

Industries Served

Aerospace & Defense
Oil & Gas
Electronics
Manufacturing
Automotive
Medical
Power Generation

Applications

  • Precision springs, snap-action switches, and contact elements in aerospace and defence electronics requiring fatigue resistance and high conductivity
  • Non-sparking tools and safety equipment for use in explosive, flammable, and volatile atmospheres in oil & gas refineries and chemical plants in UAE
  • Downhole oil & gas tools requiring high strength, non-magnetic properties, and corrosion resistance in MWD/LWD (measurement while drilling) instruments
  • Aerospace fasteners, bushings, and structural connectors requiring high strength-to-weight ratio and corrosion resistance per AMS 4534
  • Precision mould components for plastic injection moulding where exceptional thermal conductivity and high hardness must be combined
  • Electrical contact components in high-cycle switching equipment, relay springs, and connector housings requiring fatigue life and conductivity
  • Medical device components including surgical instrument springs, dental handpiece components, and implantable device connectors
  • Underwater connectors, subsea sensor housings, and ROV components requiring non-magnetic, high-strength, and corrosion-resistant properties
  • High-performance gyroscope and inertial navigation system components requiring non-magnetic copper alloy with near-steel strength
  • Resistance welding electrode faces for special applications requiring high hardness and conductivity where C18200/C18150 strength is insufficient

Chemical Composition

Cu

Copper

1.9 %
Be

Beryllium

1.8 – 2 %

0.35 %
Co+Ni

Cobalt plus Nickel

0.2 – 0.6 %

Fe

Iron

≤ 0.15 %

Si

Silicon

≤ 0.2 %

Pb

Lead

≤ 0.02 %

Other

total

≤ 0.5 %

Typical value Range (min–max) Minimum (≥) Maximum (≤) Hover / tap for notes

Standard

ASTM B197 - current edition

Available Forms

Round Bar

Diameter 3-150 mm. Extruded and drawn. Per ASTM B196 / AMS 4534 / MIL-C-21657. For precision pins, shafts, bushings, and electrical contact components. Maximum diameter smaller than steel or copper chromium grades due to beryllium processing constraints. HT (precipitation hardened) standard stock; AT (solution annealed) on request.

Flat Bar

Thickness 3-25 mm, width up to 300 mm. Per ASTM B197 / MIL-C-21657. For springs, contacts, and precision flat components in thicker sections. (Thin gauge below 3 mm is supplied as Strip.) HT and AT conditions.

Strip

Thickness 0.10-3 mm, width up to 300 mm. Per AMS 4533 / MIL-C-21657. For springs, contacts, switch elements, and precision thin-gauge flat components. HT and AT conditions.

Plate

Thickness 6-100 mm. Per ASTM B197. For mould inserts, precision tooling, and large contact components. Cut-to-size available. Smaller maximum thickness than steel due to beryllium alloy production constraints.

Block

Per ASTM B197. For mould inserts and precision tooling blocks. Cut-to-size available on indent.

Designations & Equivalents

StandardDesignationNotes
UNSC17200UNS number
EN NameCuBe2EN / DIN chemical name
EN / WerkstoffCW101CEN material code (CEN designation)
EN / Werkstoff2.1247Werkstoff-Nr. (DIN)
ASTMB197 Alloy C17200ASTM strip/plate specification
ASTMB196 Alloy C17200ASTM rod/bar specification
AMSAMS 4534C17200 rod and bar - aerospace / defence procurement reference
AMSAMS 4533C17200 strip and sheet - aerospace procurement reference
AMSMIL-C-21657C17200 rod, bar, strip, and plate - US DoD military / defence procurement reference (no MIL system in enum; mapped to AMS as the closest procurement-spec system)
ISOISO 1337 CuBe2ISO designation
Common NameBeryllium CopperCommon name
Common NameBeryllium Bronze / BeCuCommon name (variant)

Compliance & Certification

StandardStatusNotes
EN 10204 3.1SuitableEN 10204 3.1 Mill Test Certificate standard with all supply - confirms chemical composition (including Be and Co+Ni content) and mechanical properties.
EN 10204 3.2ConditionalEN 10204 3.2 independent third-party inspection available on request.
AMS 4534ConditionalAerospace rod/bar specification for C17200, available from qualified mill sources - specify clearly at enquiry stage.
AMS 4533ConditionalAerospace strip/sheet specification for C17200, available from qualified mill sources - specify clearly at enquiry stage.
MIL-C-21657ConditionalUS defence procurement specification for C17200 all wrought forms, available from qualified mill sources - specify clearly at enquiry stage. MSDS/SDS available on request for all beryllium copper supply.

Specifications

Mechanical Properties

Values are minimums unless noted; hardness is a maximum.

PropertyC17200 / CuBe2 / CW101C — ASTM B197 — Precipitation Hardened HTDefaultC17200 / CuBe2 / CW101C — ASTM B197 — Solution Annealed AT
Tensile Strength (UTS)range1170–1400 MPaTypical: 1275 MPaCondition: Room temp, longitudinalNotes: Per ASTM B197 HT. Highest commercial copper alloy. Exact value depends on prior cold work (AT+HT vs H+HT).480–690 MPaTypical: 585 MPaCondition: Room temp, longitudinalNotes: AT condition per ASTM B197. Wide range depending on exact temper and prior processing.
Yield Strength (0.2% Proof Stress)range1000–1200 MPaTypical: 1100 MPaCondition: Room tempNotes: 0.2% offset.170–380 MPaTypical: 270 MPaCondition: Room tempNotes: Low yield - maximum formability.
Elongationmin3 %Typical: 5 %Condition: 50 mm gauge lengthNotes: Low elongation in maximum strength condition.20 %Typical: 35 %Condition: 50 mm gauge lengthNotes: Excellent formability for deep drawing and complex forming.
Hardnessrange36–42 HRCTypical: 39 HRCCondition: Rockwell CNotes: HT hardness range. Approximately 352-400 HB equivalent.60–80 HRBTypical: 70 HRBCondition: Rockwell BNotes: Soft condition. Much lower than HT condition.
Electrical Conductivityrange20–25 % IACSTypical: 22 % IACSCondition: 20 degrees CNotes: Much lower than C18200/C18150. Acceptable for spring and contact applications. Higher conductivity grades (C17510) available if conductivity is critical.15–22 % IACSTypical: 18 % IACSCondition: 20 degrees CNotes: Lower than HT due to Be in solid solution. Recovers to 20-25% IACS after aging to HT.
Fatigue Strengthmax500 MPaCondition: 10^8 cycles, R=-1Notes: Outstanding fatigue life - critical for spring applications. [VERIFY]170 MPaCondition: 10^8 cycles, R=-1Notes: AT condition - lower than HT. Age to HT before final application. [VERIFY]

Physical Properties

PropertyC17200 / CuBe2 / CW101C — ASTM B197 — Precipitation Hardened HTDefaultC17200 / CuBe2 / CW101C — ASTM B197 — Solution Annealed AT
Density20 degrees C8.26 g/cm38.26 g/cm3
Modulus of Elasticity25 degrees C131 GPa131 GPa
Thermal Conductivity20 degrees C115 W/m.K115 W/m.K
Coefficient of Thermal Expansion20-100 degrees C17.8 um/m.degC17.8 um/m.degC
Specific Heat Capacity20 degrees C420 J/kg.K420 J/kg.K
Melting Point / RangeSolidus865 degrees C865 degrees C
ENGINEERING NOTES
Weldability
Not_recommended

WELDING AND FLAME CUTTING ARE STRONGLY CONTRAINDICATED for C17200. Beryllium oxide fumes generated above 650 degrees C are highly toxic and carcinogenic. If fusion welding is unavoidable in exceptional circumstances: use only in a fully enclosed, purpose-designed beryllium welding facility with LEV extraction and HEPA filtration; respiratory protection (airline supplied-air respirator) mandatory; specialist health and safety assessment required before any welding operation. In almost all applications, silver brazing (BAg-7 or equivalent at 620-680 degrees C in a fume-controlled environment) is the preferred joining method - brazing produces significantly less beryllium oxide fume than fusion welding. Never flame cut C17200 without specialist beryllium extraction equipment. Filler/joining options: AWS BAg-7 silver braze (preferred, fume-controlled environment), AWS BAg-24 silver braze (alternative for less critical joints), and ERCuBe TIG filler (specialist beryllium welding facility only, airline-supplied respirator mandatory).

Machinability
Fair

BERYLLIUM HEALTH AND SAFETY - MANDATORY READING BEFORE MACHINING OR WELDING: Beryllium fumes and dust are highly toxic. Beryllium oxide particles generated during machining, grinding, and especially welding or flame cutting can cause chronic beryllium disease (CBD) - an irreversible, debilitating lung disease - and are classified as a Group 1 human carcinogen (IARC). Engineering controls (wet machining, local exhaust ventilation with HEPA filtration), personal protective equipment (P3/N100 respirator, nitrile gloves, eye protection), and compliance with occupational exposure limits (OEL: 0.00002 mg/m3 chronic, 0.00005 mg/m3 acute - ACGIH TLV) are mandatory. All personnel must be trained in beryllium hazards before handling. Maintain MSDS/SDS on-site at all times. C17200 has good machinability in the AT (solution annealed) condition - approximately 20-30% of free-machining brass machinability index, similar to austenitic stainless steel. All machining MUST be conducted wet (flood coolant mandatory) to prevent beryllium dust generation. NEVER dry machine, dry grind, or dry polish C17200. Use water-based or synthetic coolant (not oil mist). Local exhaust ventilation with HEPA filtration is required. In the HT (hardened) condition, machinability is reduced significantly due to hardness of 36-42 HRC - carbide tooling essential. Preferred sequence: rough machine in AT condition, age to HT, then finish grind or EDM to final dimensions.

Overview

C17200 (EN CuBe2, DIN 2.1247, EN CW101C) is a copper-beryllium alloy containing 1.80-2.00% beryllium and 0.20-0.60% cobalt/nickel in a copper matrix. It is the highest-strength commercially available copper alloy, achieving tensile strengths of 1170-1400 MPa in the HT (precipitation hardened) condition - comparable to alloy steel - while maintaining electrical conductivity of 20-25% IACS and thermal conductivity far exceeding steel. The strength mechanism is analogous to other precipitation-hardening alloys: beryllium dissolves in the copper matrix during solution annealing (AT temper), then precipitates as coherent metastable particles during aging at 315-345 degrees C (HT temper), producing a dramatic increase in hardness and strength. C17200 is specified in aerospace, defence, oil & gas, and electronics applications wherever the unique combination of near-steel strength, copper-class conductivity, non-magnetic properties, non-sparking characteristics, and corrosion resistance is required. Available per AMS 4534, AMS 4533, and MIL-C-21657 for defence and aerospace procurement.

Nifty Alloys supplies C17200 / CuBe2 from stock in Dubai, UAE, in round bar, flat bar/strip, and plate/block in both the HT (precipitation hardened) and AT (solution annealed) conditions. All material is supplied with EN 10204 3.1 Mill Test Certificates as standard - confirming chemical composition, mechanical properties, and hardness. IMPORTANT: C17200 is a beryllium-containing alloy. All machining, grinding, and processing must be conducted in compliance with applicable occupational health and safety regulations (COSHH, UAE Federal Law No. 8, OSHA 29 CFR 1910.1024 as applicable). Nifty Alloys provides material safety data sheets (MSDS/SDS) upon request. We deliver across the UAE within 24-48 hours and export to Saudi Arabia, Kuwait, Qatar, Oman, and Bahrain.

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C17200 (CuBe2, CW101C, 2.1247) is the highest-strength commercially available copper alloy, specified wherever near-steel strength, high conductivity, and non-sparking or non-magnetic properties must be combined. Key applications in UAE and globally include: non-sparking tools and safety equipment for explosive and flammable atmospheres in oil & gas and chemical facilities; precision springs, snap-action switches, and electrical contacts in aerospace and defence electronics; downhole oil & gas MWD/LWD instrument components requiring high strength and non-magnetic properties; aerospace fasteners and structural connectors per AMS 4534; precision mould inserts requiring high hardness and thermal conductivity; subsea connectors and sensor housings for offshore oil & gas; medical device springs and dental handpiece components; and resistance welding electrode faces for special high-hardness applications. Its unique combination of properties makes it irreplaceable in applications where no other material satisfies all requirements simultaneously.

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