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Copper Alloy QBe1.9-TM02

Precip hard

GB QBe1.9

TM02 = mill hardened, half hard

Mill-hardened strip supplied ready to stamp — no customer aging, dimensionally stable, moderate strength with good formability.

High cost $$$$

Values for the TM02 condition

Other QBe1.9 tempers and conditions

QBe1.9 is listed in 12 conditions; see the grade overview at QBe1.9.

Compare all 12 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution heat treated
Softest condition — pick for deep drawing, stamping and complex forming before customer-side age hardening.24048045105 HB17 % IACS
Solution heat treated and cold worked, quarter hard
Light cold work for moderate forming plus a small pre-age strength boost.45056028150 HB17 % IACS
Solution heat treated and cold worked, half hard
Balanced strength/formability strip and rod for parts formed with modest bend radii before aging.58564015190 HB17 % IACS
three-quarter hard, cold worked
Intermediate step between half and full hard for flat springs needing limited forming.640700915 HRC17 % IACS
TM02This page
Mill hardened, half hard
Mill-hardened strip supplied ready to stamp — no customer aging, dimensionally stable, moderate strength with good formability.6908301227 HRC20 % IACS
Solution heat treated and cold worked, full hard
Maximum pre-age cold work — highest strength before aging, used for flat springs and blanked contacts.720780521 HRC17 % IACS
Mill hardened, extra hard
High-strength mill-hardened strip for high-force connector springs where post-form aging is not practical.9651,070634 HRC21 % IACS
TF00Default
Solution heat treated and precipitation hardened
Standard peak-aged condition for machined parts, moulds, bushings and non-sparking tools — best strength/ductility balance.1,0701,240539 HRC23 % IACS
TD01 and precipitation hardened
Cold worked 1/4 hard then aged — slightly stronger than AT while retaining useful ductility.1,1201,275440 HRC23 % IACS
TD02 and precipitation hardened
Standard high-strength spring strip condition for connectors and contact fingers.1,1901,330442 HRC23 % IACS
three-quarter hard then aged
Intermediate aged spring temper where TH04 would be too brittle for the bend radius.1,2401,380343 HRC24 % IACS
TD04 and precipitation hardened
Maximum strength and hardness of the alloy — flat springs, diaphragms and Bourdon tubes with minimal forming after aging.1,2401,380243 HRC23 % IACS

What is QBe1.9-TM02?

QBe1.9-TM02 is QBe1.9 in the TM02 condition — mill-hardened strip supplied ready to stamp — no customer aging, dimensionally stable, moderate strength with good formability. QBe1.9-TM02 has a yield strength of 690 MPa (100 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 96% of copper alloy grades. Elongation at break is 12% and the elastic modulus is 128 GPa (18.6 Msi). QBe1.9-TM02 has a density of 8.26 g/cm³ (0.298 lb/in³), lighter than 83% of copper alloy grades. It melts at 865°C (1,589 °F). TF00 is the default condition FabDigit quotes; TM02 is available on request or by drawing note.

Advantages

  • High strength — 690 MPa (100 ksi), better than 96% of copper alloy grades
  • Polishes to a fine finish — 85/100, better than 92% of copper alloy grades
  • Tough — resists crack growth — 55 MPa·√m (50.1 ksi·√in), better than 85% of copper alloy grades

Limitations

  • High embodied carbon — 7.5 kg CO₂/kg, worse than 97% of copper alloy grades

QBe1.9-TM02 properties

Typical room-temperature values for QBe1.9-TM02; 23 are specific to this condition. Other listed values are QBe1.9 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

QBe1.9-TM02 has a density of 8.26 g/cm³ (0.298 lb/in³), lighter than 83% of copper alloy grades. It melts at 865°C (1,589 °F).

Density8.26 g/cm³0.3 lb/in³
Melting Point (Solidus)865°C1,589 °F
Liquidus Temperature980°C1,796 °F

Mechanical16

QBe1.9-TM02 has a yield strength of 690 MPa (100 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 96% of copper alloy grades. Elongation at break is 12% and the elastic modulus is 128 GPa (18.6 Msi).

Elastic (Young's) Modulus128 GPa18.6 Msi
Shear Modulus50 GPa7.3 Msi
Bulk Modulus108 GPa15.7 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)830 MPa120 ksi
Yield Strength (0.2% offset)690 MPa100 ksi
Elongation at Break12%
Reduction in Area30%
Compressive Strength730 MPa106 ksi
Shear Strength525 MPa76.1 ksi
Fatigue Strength (Endurance Limit)240 MPa34.8 ksi
Fracture Toughness (K_IC)55 MPa·√m50.1 ksi·√in
Charpy V-Notch Impact (RT)18 J13.3 ft·lbf
Hardness, Brinell265 HB
Hardness, Rockwell C27 HRC
Hardness, Vickers275 HV

Thermal6

QBe1.9-TM02 is rated for continuous service to 200°C (392 °F). It conducts heat at 100 W/m·K (57.8 BTU/hr·ft·°F), better than 54% of copper alloy grades. Thermal expansion is 17 µm/m·K (9.44 µin/in·°F).

Thermal Conductivity100 W/m·K57.8 BTU/hr·ft·°F
Specific Heat Capacity420 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

QBe1.9-TM02 conducts electricity at 20 % IACS, better than 52% of copper alloy grades.

Electrical Conductivity20 % IACS
Electrical Resistivity8.6×10⁻⁸ Ω·m3.39 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (62/100), worse than 57% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.24 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood in fresh and sea water, mild acids and industrial atmospheres; attacked by ammonia/amines, oxidising acids, hydrogen sulfide and cyanides; less prone to stress-corrosion cracking than brasses.

Sustainability4

Producing a kilogram of QBe1.9-TM02 takes about 105 MJ of energy and emits 7.5 kg of CO₂ — more than 97% of copper alloy grades. Typical recycled content is 25%.

Embodied Energy (primary production)105 MJ/kg45,142 BTU/lb
Embodied Carbon (primary production)7.5 kg CO₂/kg
Embodied Water480 L/kg57.5 gal/lb
Typical Recycled Content25%

Manufacturability8

QBe1.9-TM02's machinability is fair (39/100, better than 55% of copper alloy grades); weldability fair (45/100); formability fair (45/100).

MachinabilityFair39/100
Machinability Rating (AISI 1212 = 100 %)23%
WeldabilityFair45/100
Formability (cold)Fair45/100
CastabilityGood55/100
Brazeability / SolderabilityVery good75/100
PolishabilityExcellent85/100
Anodizing Responsen/a — copper alloy; use passivation, tin/nickel/gold plating or chromate-free tarnish inhibitors

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

Working with QBe1.9-TM02

Is QBe1.9 easy to machine?

Machine in TB00/TD tempers where possible; aged material cuts like 40 HRC steel — use carbide, rigid setups, flood coolant and full dust/fume capture for beryllium.

Can QBe1.9 be welded?

Resistance and electron-beam welding are routine; TIG is possible with matched filler and inert shielding, but the weld zone must be re-solution treated and re-aged, and fume extraction is mandatory.

Can QBe1.9 be formed, bent or molded?

Do all deep drawing, bending and coiling in the solution-annealed or cold-worked temper, then age at 315–330 °C for 2–3 h (allow ~0.2 % dimensional contraction); aged stock has very limited formability.

What surface finishes work on QBe1.9?

Not anodizable; degrease and pickle to remove the aging oxide, then nickel, tin or gold plate for contacts, or polish to mirror finish for mould inserts.

QBe1.9 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
Beprincipal hardening element1.85 – 2.11.95
Nigrain refiner / aging control0.2 – 0.40.3
Ti0.1 – 0.250.18
Alimpurity limit≤ 0.15—
Feimpurity limit≤ 0.15—
Siimpurity limit≤ 0.15—
Pbimpurity limit≤ 0.01—
Curemainder, total impurities ≤ 0.5 %balance—

QBe1.9-TM02 — frequently asked

What is QBe1.9-TM02 used for?

QBe1.9-TM02 is typically used for precision springs, electrical contacts, molds and non-sparking tools. In short: highest-strength copper alloy; spring and mould-insert grade; requires beryllium dust control.

What is the yield strength of QBe1.9-TM02?

QBe1.9-TM02 has a typical yield strength of 690 MPa (100 ksi) and a tensile strength of 830 MPa (120 ksi) — stronger than 96% of copper alloy grades. Strength varies by condition: see the 12 listed tempers.

Is QBe1.9-TM02 easy to machine?

Not especially — machinability is rated fair (39/100, better than 55% of copper alloy grades). Machine in TB00/TD tempers where possible; aged material cuts like 40 HRC steel — use carbide, rigid setups, flood coolant and full dust/fume capture for beryllium.

Can QBe1.9-TM02 be welded?

With care — weldability is rated fair (45/100). Resistance and electron-beam welding are routine; TIG is possible with matched filler and inert shielding, but the weld zone must be re-solution treated and re-aged, and fume extraction is mandatory.

What surface finishes work on QBe1.9-TM02?

Not anodizable; degrease and pickle to remove the aging oxide, then nickel, tin or gold plate for contacts, or polish to mirror finish for mould inserts.

Can QBe1.9-TM02 be formed, bent or molded?

Do all deep drawing, bending and coiling in the solution-annealed or cold-worked temper, then age at 315–330 °C for 2–3 h (allow ~0.2 % dimensional contraction); aged stock has very limited formability.

What is the maximum service temperature of QBe1.9-TM02?

QBe1.9-TM02 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 QBe1.9-TF00 and QBe1.9-TB00?

TF00 is the default condition — standard peak-aged condition for machined parts, moulds, bushings and non-sparking tools — best strength/ductility balance. TB00: softest condition — pick for deep drawing, stamping and complex forming before customer-side age hardening. Yield strength is 1,070 MPa in TF00 versus 240 MPa in TB00.

Sources

  1. C17200 Alloy Datasheet — Copper Development Association (copper.org) (2023)
  2. Alloy 25 (C17200) Strip and Rod Technical Data — Materion Brush Performance Alloys (2021)
  3. 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.