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Refractory Metal C-129Y-SR (Stress relieved)

Heat-treated state

UNS R04360

Choose when higher room-temperature strength is wanted with usable ductility and dimensional stability after forming.

High cost $$$$

Values for the SR 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
AnnealedDefault
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
SRThis page
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-SR?

C-129Y-SR is C-129Y heat treated to SR — choose when higher room-temperature strength is wanted with usable ductility and dimensional stability after forming. C-129Y-SR has a yield strength of 620 MPa (89.9 ksi) and a tensile strength of 700 MPa (102 ksi) — stronger than 84% of refractory metal grades. Elongation at break is 12% and the elastic modulus is 131 GPa (19 Msi). C-129Y-SR 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). Annealed is the default condition FabDigit quotes; SR is available on request or by drawing note.

Advantages

  • Tough — resists crack growth — 72 MPa·√m (65.5 ksi·√in), better than 88% of refractory metal grades
  • High strength — 620 MPa (89.9 ksi), better than 84% of refractory metal grades
  • High service temperature — 1,300°C (2,372 °F), better than 76% of refractory metal grades

C-129Y-SR properties

Typical room-temperature values for C-129Y-SR; 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-SR 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-SR has a yield strength of 620 MPa (89.9 ksi) and a tensile strength of 700 MPa (102 ksi) — stronger than 84% of refractory metal grades. Elongation at break is 12% 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)700 MPa102 ksi
Yield Strength (0.2% offset)620 MPa89.9 ksi
Elongation at Break12%
Reduction in Area30%
Compressive Strength630 MPa91.4 ksi
Shear Strength430 MPa62.4 ksi
Fatigue Strength (Endurance Limit)340 MPa49.3 ksi
Fracture Toughness (K_IC)72 MPa·√m65.5 ksi·√in
Charpy V-Notch Impact (RT)25 J18.4 ft·lbf
Hardness, Brinell247 HB
Hardness, Rockwell B100 HRB
Hardness, Rockwell C24 HRC
Hardness, Vickers260 HV

Thermal6

C-129Y-SR is rated for continuous service to 1,300°C (2,372 °F). It conducts heat at 31 W/m·K (17.9 BTU/hr·ft·°F), worse than 59% of refractory metal grades. Thermal expansion is 7.5 µm/m·K (4.17 µin/in·°F).

Thermal Conductivity31 W/m·K17.9 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)1,300°C2,372 °F
Min Service Temperature-253°C-423 °F

Electrical3

C-129Y-SR conducts electricity at 3.5 % IACS, worse than 70% of refractory metal grades.

Electrical Conductivity3.5 % IACS
Electrical Resistivity4.9×10⁻⁷ Ω·m19.3 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-SR 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-SR's machinability is poor (22/100, worse than 73% of refractory metal grades); weldability good (65/100); formability fair (45/100).

MachinabilityPoor22/100
Machinability Rating (AISI 1212 = 100 %)18%
WeldabilityGood65/100
Formability (cold)Fair45/100
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.

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

Working with C-129Y-SR

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-SR — frequently asked

What is C-129Y-SR used for?

C-129Y-SR 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-SR?

C-129Y-SR has a typical yield strength of 620 MPa (89.9 ksi) and a tensile strength of 700 MPa (102 ksi) — stronger than 84% of refractory metal grades. Strength varies by condition: see the 3 listed tempers.

Is C-129Y-SR easy to machine?

Not especially — machinability is rated poor (22/100, worse than 73% 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-SR be welded?

Yes — weldability is rated good (65/100). 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-SR?

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-SR 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-SR?

C-129Y-SR is rated for continuous use to about 1,300°C (2,372 °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.