FabDigitFabDigit

Refractory Metal C-129Y Annealed

Temper · default condition

UNS R04360

Standard stocked condition for sheet and plate: best ductility and formability, baseline strength for hot-structure design.

High cost $$$$

Values for the Annealed condition

Other C-129Y tempers and conditions

C-129Y is listed in 3 conditions; see the grade overview at C-129Y.

Compare all 3 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
AnnealedDefaultThis page
recrystallization annealed sheet/plate (vacuum, ~1300–1500 °C)
Standard stocked condition for sheet and plate: best ductility and formability, baseline strength for hot-structure design.4805852218 HRC3.6 % IACS
Stress relieved
Choose when higher room-temperature strength is wanted with usable ductility and dimensional stability after forming.6207001224 HRC3.5 % IACS
Cold worked
Maximum room-temperature strength for thin sheet, foil and wire where no high-temperature exposure will recrystallize the material.830900630 HRC3.4 % IACS

What is C-129Y Annealed?

C-129Y Annealed is C-129Y in the Annealed temper — standard stocked condition for sheet and plate: best ductility and formability, baseline strength for hot-structure design. C-129Y Annealed has a yield strength of 480 MPa (69.6 ksi) and a tensile strength of 585 MPa (84.8 ksi) — stronger than 72% of refractory metal grades. Elongation at break is 22% and the elastic modulus is 131 GPa (19 Msi). C-129Y Annealed has a density of 9.46 g/cm³ (0.342 lb/in³), heavier than 59% of refractory metal grades. It melts at 2,450°C (4,442 °F).

Advantages

  • Tough — resists crack growth — 90 MPa·√m (81.9 ksi·√in), better than 94% of refractory metal grades
  • High service temperature — 1,400°C (2,552 °F), better than 81% of refractory metal grades

C-129Y Annealed properties

Typical room-temperature values for C-129Y Annealed; 23 are specific to this condition. Other listed values are C-129Y reference data and may not represent this condition. Bars are the position among refractory metal grades.

Physical3

C-129Y Annealed has a density of 9.46 g/cm³ (0.342 lb/in³), heavier than 59% of refractory metal grades. It melts at 2,450°C (4,442 °F).

Density9.46 g/cm³0.34 lb/in³
Melting Point (Solidus)2,450°C4,442 °F
Liquidus Temperature2,520°C4,568 °F

Mechanical17

C-129Y Annealed has a yield strength of 480 MPa (69.6 ksi) and a tensile strength of 585 MPa (84.8 ksi) — stronger than 72% of refractory metal grades. Elongation at break is 22% and the elastic modulus is 131 GPa (19 Msi).

Elastic (Young's) Modulus131 GPa19 Msi
Shear Modulus48 GPa7 Msi
Bulk Modulus165 GPa23.9 Msi
Poisson's Ratio0.36
Tensile Strength (Ultimate)585 MPa84.8 ksi
Yield Strength (0.2% offset)480 MPa69.6 ksi
Elongation at Break22%
Reduction in Area45%
Compressive Strength490 MPa71.1 ksi
Shear Strength360 MPa52.2 ksi
Fatigue Strength (Endurance Limit)280 MPa40.6 ksi
Fracture Toughness (K_IC)90 MPa·√m81.9 ksi·√in
Charpy V-Notch Impact (RT)40 J29.5 ft·lbf
Hardness, Brinell209 HB
Hardness, Rockwell B95 HRB
Hardness, Rockwell C18 HRC
Hardness, Vickers220 HV

Thermal6

C-129Y Annealed is rated for continuous service to 1,400°C (2,552 °F). It conducts heat at 32 W/m·K (18.5 BTU/hr·ft·°F), worse than 58% of refractory metal grades. Thermal expansion is 7.5 µm/m·K (4.17 µin/in·°F).

Thermal Conductivity32 W/m·K18.5 BTU/hr·ft·°F
Specific Heat Capacity270 J/kg·K0.06 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)7.5 µm/m·K4.2 µin/in·°F
Latent Heat of Fusion285 J/g123 BTU/lb
Max Service Temperature (continuous)1,400°C2,552 °F
Min Service Temperature-253°C-423 °F

Electrical3

C-129Y Annealed conducts electricity at 3.6 % IACS, worse than 68% of refractory metal grades.

Electrical Conductivity3.6 % IACS
Electrical Resistivity4.8×10⁻⁷ Ω·m18.9 µΩ·in
Magnetic Responsenon-magnetic (paramagnetic)

Chemical & Environmental3

Corrosion resistance is good (68/100), worse than 63% of refractory metal grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceGood68/100
Chemical Resistance SummaryVery resistant at ambient temperature to most mineral acids (HCl, HNO₃, H₂SO₄), chlorides and liquid alkali metals; attacked by HF, hot concentrated alkali and fluoride media, and oxidizes catastrophically in air above ~400–500 °C so an oxidation-resistant silicide coating is required for air service.

Sustainability4

Producing a kilogram of C-129Y Annealed takes about 620 MJ of energy and emits 42 kg of CO₂ — less than 67% of refractory metal grades. Typical recycled content is 25%.

Embodied Energy (primary production)620 MJ/kg266,552 BTU/lb
Embodied Carbon (primary production)42 kg CO₂/kg
Embodied Water900 L/kg108 gal/lb
Typical Recycled Content25%

Manufacturability7

C-129Y Annealed's machinability is poor (25/100, worse than 65% of refractory metal grades); weldability very good (70/100); formability good (65/100).

MachinabilityPoor25/100
Machinability Rating (AISI 1212 = 100 %)20%
WeldabilityVery good70/100
Formability (cold)Good65/100
Brazeability / SolderabilityGood55/100
PolishabilityGood60/100
Anodizing Responsen/a for structural use — niobium anodizes to decorative interference oxide films but this is not a service coating; silicide (R512E) or aluminide coatings are used for oxidation protection.

Common Calculations5

Specific Strength (UTS / density)calculated62 kN·m/kg
Specific Stiffness (E / density)calculated13.8 MN·m/kg
Modulus of Resiliencecalculated879 kJ/m³
Thermal Diffusivitycalculated12.5 mm²/s
Thermal Shock Resistance Indexcalculated19

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

Working with C-129Y Annealed

Is C-129Y easy to machine?

Machine slow with sharp, positive-rake carbide or HSS-Co tooling, heavy rigid setups and flood coolant; it work-hardens and galls, so avoid dwell and take positive chip loads.

Can C-129Y be welded?

GTAW or EB weld in vacuum or high-purity argon with full backside shielding — oxygen/nitrogen pickup embrittles the weld; clean and degrease thoroughly and post-weld vacuum anneal where possible.

Can C-129Y be formed, bent or molded?

Sheet forms readily cold in the annealed condition with generous bend radii; heavy sections are worked warm (600–1000 °C) and vacuum annealed between passes.

What surface finishes work on C-129Y?

Chemically clean (HNO₃-HF pickle) then apply a fused silicide coating such as R512E for oxidation protection; decorative anodizing is possible but has no service value.

C-129Y 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
Wsolid-solution strengthener9 – 1110
Hfcarbide/oxide strengthening, coating adherence9 – 1110
Yinterstitial scavenger0.05 – 0.150.1
Zrresidual from Hf≤ 0.5—
Taresidual≤ 0.5—
C≤ 0.030.01
O≤ 0.020.01
N≤ 0.010.01
H≤ 0—
Fe≤ 0.05—
Nbbalance—

C-129Y Annealed — frequently asked

What is C-129Y Annealed used for?

C-129Y Annealed is typically used for rocket nozzle extensions, high-temperature structural panels and re-entry vehicle components. In short: stronger creep than C-103; yttrium-doped Nb-W-Hf sheet; needs silicide coating in air.

What is the yield strength of C-129Y Annealed?

C-129Y Annealed has a typical yield strength of 480 MPa (69.6 ksi) and a tensile strength of 585 MPa (84.8 ksi) — stronger than 72% of refractory metal grades. Strength varies by condition: see the 3 listed tempers.

Is C-129Y Annealed easy to machine?

Not especially — machinability is rated poor (25/100, worse than 65% of refractory metal grades). Machine slow with sharp, positive-rake carbide or HSS-Co tooling, heavy rigid setups and flood coolant; it work-hardens and galls, so avoid dwell and take positive chip loads.

Can C-129Y Annealed be welded?

Yes — weldability is rated very good (70/100). GTAW or EB weld in vacuum or high-purity argon with full backside shielding — oxygen/nitrogen pickup embrittles the weld; clean and degrease thoroughly and post-weld vacuum anneal where possible.

What surface finishes work on C-129Y Annealed?

Chemically clean (HNO₃-HF pickle) then apply a fused silicide coating such as R512E for oxidation protection; decorative anodizing is possible but has no service value.

Can C-129Y Annealed be formed, bent or molded?

Sheet forms readily cold in the annealed condition with generous bend radii; heavy sections are worked warm (600–1000 °C) and vacuum annealed between passes.

What is the maximum service temperature of C-129Y Annealed?

C-129Y Annealed is rated for continuous use to about 1,400°C (2,552 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C-129Y Annealed and C-129Y-CW?

Annealed is the default condition — standard stocked condition for sheet and plate: best ductility and formability, baseline strength for hot-structure design. CW: maximum room-temperature strength for thin sheet, foil and wire where no high-temperature exposure will recrystallize the material. Yield strength is 480 MPa in Annealed versus 830 MPa in CW.

Sources

  1. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose Materials, refractory metals section — ASM International (1990)
  2. Aerospace Structural Metals Handbook — niobium (columbium) alloys — CINDAS/Purdue (1999)
  3. ASTM B652/B654 — Niobium-alloy bar, rod, sheet, strip and foil — ASTM International (2019)
  4. Refractory metal alloy datasheets (Nb-10W-10Hf-0.1Y, C-103, Cb-752) — specialty refractory metal producers (2023)

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.