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Refractory Metal C-103 · heat-treated state · default condition

Refractory Metal C-103 Vacuum Annealed

Properties of the Vacuum Annealed condition, compared with the other C-103 tempers.

Standard stocked condition for sheet/plate/bar that must be deep-drawn, spun or welded into thruster nozzles.

CNC machiningSheet metalSpecialty cost $$$$$

What is C-103 Vacuum Annealed?

C-103 Vacuum Annealed is C-103 heat treated to Vacuum Annealed — standard stocked condition for sheet/plate/bar that must be deep-drawn, spun or welded into thruster nozzles. C-103 Vacuum Annealed has a yield strength of 275 MPa (39.9 ksi) and a tensile strength of 415 MPa (60.2 ksi) — weaker than 65% of refractory metal grades. Elongation at break is 25% and the elastic modulus is 88 GPa (12.8 Msi). C-103 Vacuum Annealed has a density of 8.85 g/cm³ (0.32 lb/in³), heavier than 56% of refractory metal grades. It melts at 2,350°C (4,262 °F).

Advantages

  • Readily welded — 80/100, better than 92% of refractory metal grades
  • Forms and bends easily — 85/100, better than 87% of refractory metal grades
  • High service temperature — 1,400°C (2,552 °F), better than 79% of refractory metal grades

Limitations

  • Low stiffness — 88 GPa (12.8 Msi), worse than 99% of refractory metal grades

C-103 Vacuum Annealed properties

Typical room-temperature values for C-103 Vacuum Annealed — 10 properties are specific to this condition; the rest are grade-level values shared by every C-103 temper. Each bar shows where the value sits among the refractory metal grades in FabDigit's library — further right is higher.

Physical3

C-103 Vacuum Annealed has a density of 8.85 g/cm³ (0.32 lb/in³), heavier than 56% of refractory metal grades. It melts at 2,350°C (4,262 °F).

Density8.85 g/cm³0.32 lb/in³
Melting Point (Solidus)2,350°C4,262 °F
Liquidus Temperature2,400°C4,352 °F

Mechanical12

C-103 Vacuum Annealed has a yield strength of 275 MPa (39.9 ksi) and a tensile strength of 415 MPa (60.2 ksi) — weaker than 65% of refractory metal grades. Elongation at break is 25% and the elastic modulus is 88 GPa (12.8 Msi).

Elastic (Young's) Modulus88 GPa12.8 Msi
Shear Modulus33 GPa4.8 Msi
Bulk Modulus98 GPa14.2 Msi
Poisson's Ratio0.35
Tensile Strength (Ultimate)415 MPa60.2 ksi
Yield Strength (0.2% offset)275 MPa39.9 ksi
Elongation at Break25%
Reduction in Area55%
Shear Strength250 MPa36.3 ksi
Fatigue Strength (Endurance Limit)200 MPa29 ksi
Hardness, Rockwell B85 HRB
Hardness, Vickers180 HV

Thermal6

C-103 Vacuum Annealed is rated for continuous service to 1,400°C (2,552 °F). It conducts heat at 42 W/m·K (24.3 BTU/hr·ft·°F), better than 50% of refractory metal grades. Thermal expansion is 7.4 µm/m·K (4.11 µin/in·°F).

Thermal Conductivity42 W/m·K24.3 BTU/hr·ft·°F
Specific Heat Capacity272 J/kg·K0.06 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)7.4 µm/m·K4.1 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-103 Vacuum Annealed conducts electricity at 5.1 % IACS, worse than 59% of refractory metal grades.

Electrical Conductivity5.1 % IACS
Electrical Resistivity3.4×10⁻⁷ Ω·m13.4 µΩ·in
Magnetic Responsenon-magnetic (paramagnetic)

Chemical & Environmental3

Corrosion resistance is good (62/100), worse than 66% of refractory metal grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryPassive and highly resistant in most mineral acids, chlorides and liquid alkali metals (Na, K, Li); attacked by HF, fluorides, hot concentrated alkalis; absorbs H, O and N above ~250–400 °C, so bare service in air is limited to ~400 °C.

Sustainability3

Producing a kilogram of C-103 Vacuum Annealed takes about 900 MJ of energy and emits 55 kg of CO₂ — less than 59% of refractory metal grades. Typical recycled content is 25%.

Embodied Energy (primary production)900 MJ/kg386,931 BTU/lb
Embodied Carbon (primary production)55 kg CO₂/kg
Typical Recycled Content25%

Manufacturability8

C-103 Vacuum Annealed's machinability is poor (30/100, better than 55% of refractory metal grades); weldability very good (80/100); formability excellent (85/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)25%
WeldabilityVery good80/100
Formability (cold)Excellent85/100
CastabilityPoor20/100
Brazeability / SolderabilityGood60/100
PolishabilityGood60/100
Anodizing Responsen/a for decorative use; Nb anodizes to interference colours in dilute electrolytes, but service protection is by R512E silicide or Si–Cr–Fe slurry coating

Common Calculations5

Specific Strength (UTS / density)calculated47 kN·m/kg
Specific Stiffness (E / density)calculated9.9 MN·m/kg
Modulus of Resiliencecalculated430 kJ/m³
Thermal Diffusivitycalculated17.4 mm²/s
Thermal Shock Resistance Indexcalculated27

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other C-103 tempers and conditions

C-103 is also supplied in 3 other conditions. The full side-by-side table is on the C-103 overview.

Working with C-103 Vacuum Annealed

Is C-103 easy to machine?

Gummy and galling like tantalum — use sharp, high-positive-rake carbide or HSS tools, slow speed, heavy feed, generous chlorinated or water-soluble coolant, and avoid dwelling; grind with SiC and plenty of coolant.

Can C-103 be welded?

Excellent GTAW/EBW/laser weldability, but only in vacuum or high-purity inert chambers/trailing shields — any O, N or H pickup embrittles the weld; clean and pickle before welding, no filler usually needed.

Can C-103 be formed, bent or molded?

Very ductile cold: deep draws, spins and rolls readily with clean tooling and non-chlorinated lubricant; interstage vacuum anneals restore ductility, and hot working is done above ~1100 °C under protection.

What surface finishes work on C-103?

Chemically pickle (HNO₃/HF) then apply R512E silicide or Si-Cr slurry coating for oxidation service; electropolishing and anodic colouring are possible but coating adhesion prep governs flight hardware.

C-103 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
Hf9 – 1110
Ti0.7 – 1.31
Zrresidual from Hf source≤ 0.70.5
Ta≤ 0.5
W≤ 0.5
C≤ 0.02
O≤ 0.03
N≤ 0.01
H≤ 0
Fe≤ 0.01
Ni≤ 0.01
Si≤ 0.01
Nbbalance

C-103 Vacuum Annealed — frequently asked

What is C-103 Vacuum Annealed used for?

C-103 Vacuum Annealed is typically used for rocket nozzle extensions and inserts, spacecraft thruster combustion chambers, rocket engine thrust chamber liners, hot gas structures and leading edges, radiation shields and heat shields and high-temperature furnace fixtures. In short: aerospace high-temp niobium.

What is the yield strength of C-103 Vacuum Annealed?

C-103 Vacuum Annealed has a typical yield strength of 275 MPa (39.9 ksi) and a tensile strength of 415 MPa (60.2 ksi) — weaker than 65% of refractory metal grades. Strength varies by condition: see the 4 listed tempers.

Is C-103 Vacuum Annealed easy to machine?

Not especially — machinability is rated poor (30/100, better than 55% of refractory metal grades). Gummy and galling like tantalum — use sharp, high-positive-rake carbide or HSS tools, slow speed, heavy feed, generous chlorinated or water-soluble coolant, and avoid dwelling; grind with SiC and plenty of coolant.

Can C-103 Vacuum Annealed be welded?

Yes — weldability is rated very good (80/100). Excellent GTAW/EBW/laser weldability, but only in vacuum or high-purity inert chambers/trailing shields — any O, N or H pickup embrittles the weld; clean and pickle before welding, no filler usually needed.

What surface finishes work on C-103 Vacuum Annealed?

Chemically pickle (HNO₃/HF) then apply R512E silicide or Si-Cr slurry coating for oxidation service; electropolishing and anodic colouring are possible but coating adhesion prep governs flight hardware.

Can C-103 Vacuum Annealed be formed, bent or molded?

Very ductile cold: deep draws, spins and rolls readily with clean tooling and non-chlorinated lubricant; interstage vacuum anneals restore ductility, and hot working is done above ~1100 °C under protection.

What is the maximum service temperature of C-103 Vacuum Annealed?

C-103 Vacuum 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.

Can FabDigit make parts in C-103 Vacuum Annealed?

Yes — C-103 Vacuum Annealed is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. ASTM B654 — Niobium-Hafnium Alloy Foil, Sheet, Strip and PlateASTM International (2020)
  2. ASTM B652 — Niobium-Hafnium Alloy IngotsASTM International (2020)
  3. ASTM B655 — Niobium-Hafnium Alloy Bar, Rod and WireASTM International (2020)
  4. ASM Handbook Vol. 2 — Properties of Refractory Metals and AlloysASM International (1990)
  5. C-103 (Nb-10Hf-1Ti) alloy datasheetATI / Wah Chang refractory metals (2019)
  6. Refractory-metal nozzle materials and R512E coating performance summariesNASA technical reports (1972)

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.