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TD-Nickel REX

Heat-treated state

UNS N02120 · also TD Nickel

REX = high-temperature recrystallized (coarse elongated grain) condition

Pick when maximum creep-rupture life above 1100 °C matters more than room-temperature strength; the coarse elongated grain structure minimises grain-boundary sliding.

High cost $$$$

Values for the REX condition

Other TD-Nickel grades and fills

TD-Nickel is listed in 2 conditions; see the grade overview at TD-Nickel.

Compare all 2 grades and fillsHide
Grade · open for datasheetBest forYield MPaTensile MPaElong. %Hardness
REXThis page
High-temperature recrystallized (coarse elongated grain) condition
Pick when maximum creep-rupture life above 1100 °C matters more than room-temperature strength; the coarse elongated grain structure minimises grain-boundary sliding.27040022—
Ni-20Cr-2ThO₂ chromium-bearing version
Choose when bare-surface oxidation resistance is required above 1000 °C without a coating; higher strength but lower thermal conductivity than TD-Ni.56070014—

What is TD-Nickel REX?

TD-Nickel REX is TD-Nickel heat treated to REX — pick when maximum creep-rupture life above 1100 °C matters more than room-temperature strength; the coarse elongated grain structure minimises grain-boundary sliding. TD-Nickel REX has a yield strength of 270 MPa (39.2 ksi) and a tensile strength of 400 MPa (58 ksi) — weaker than 58% of composite grades. Elongation at break is 22% and the elastic modulus is 207 GPa (30 Msi). TD-Nickel REX has a density of 8.9 g/cm³ (0.322 lb/in³), heavier than 98% of composite grades.

Advantages

  • Ductile — tolerates forming and impact — 22%, better than 98% of composite grades
  • High service temperature — 1,250°C (2,282 °F), better than 96% of composite grades
  • Good UV / weathering resistance — 100/100, better than 93% of composite grades
  • Conducts heat well — 67 W/m·K (38.7 BTU/hr·ft·°F), better than 87% of composite grades
  • Polishes to a fine finish — 55/100, better than 83% of composite grades

Limitations

  • Heavy — 8.9 g/cm³ (0.322 lb/in³), worse than 98% of composite grades
  • Needs corrosion protection — 55/100, worse than 87% of composite grades

TD-Nickel REX properties

Typical room-temperature values for TD-Nickel REX; 12 are specific to this condition. Other listed values are TD-Nickel reference data and may not represent this condition. Bars are the position among composite grades.

Physical1

TD-Nickel REX has a density of 8.9 g/cm³ (0.322 lb/in³), heavier than 98% of composite grades.

Density8.9 g/cm³0.32 lb/in³

Mechanical8

TD-Nickel REX has a yield strength of 270 MPa (39.2 ksi) and a tensile strength of 400 MPa (58 ksi) — weaker than 58% of composite grades. Elongation at break is 22% and the elastic modulus is 207 GPa (30 Msi).

Elastic (Young's) Modulus207 GPa30 Msi
Shear Modulus78 GPa11.3 Msi
Bulk Modulus180 GPa26.1 Msi
Poisson's Ratio0.31
Tensile Strength (Ultimate)400 MPa58 ksi
Yield Strength (0.2% offset)270 MPa39.2 ksi
Elongation at Break22%
Shear Strength265 MPa38.4 ksi

Thermal6

TD-Nickel REX is rated for continuous service to 1,250°C (2,282 °F). It conducts heat at 67 W/m·K (38.7 BTU/hr·ft·°F), better than 87% of composite grades. Thermal expansion is 13.3 µm/m·K (7.39 µin/in·°F).

Thermal Conductivity67 W/m·K38.7 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)13.3 µm/m·K7.4 µin/in·°F
Max Service Temperature (continuous)1,250°C2,282 °F
Min Service Temperature-200°C-328 °F
Max Service Temperature (short-term)1,370°C2,498 °F

Electrical1

TD-Nickel REX has an electrical resistivity of 9.3×10⁻⁸ Ω·m.

Electrical Resistivity9.3×10⁻⁸ Ω·m3.66 µΩ·in

Chemical & Environmental3

Corrosion resistance is good (55/100), worse than 87% of composite grades. UV resistance is excellent.

Corrosion ResistanceGood55/100
UV / Weathering ResistanceExcellent100/100
Chemical Resistance SummaryBehaves like commercially pure nickel: excellent in caustics, neutral salts and reducing acids; poor in oxidizing acids (HNO₃) and ammonia/sulfur-bearing hot gases; bare Ni matrix oxidizes/spalls above ~1000 °C in air so aluminide or Cr-rich coatings are normally applied.

Sustainability4

Producing a kilogram of TD-Nickel REX takes about 230 MJ of energy and emits 17 kg of CO₂ — more than 52% of composite grades. Typical recycled content is 0%.

Embodied Energy (primary production)230 MJ/kg98,882 BTU/lb
Embodied Carbon (primary production)17 kg CO₂/kg
Embodied Water250 L/kg30 gal/lb
Typical Recycled Content0%

Manufacturability2

TD-Nickel REX's machinability is poor (28/100, worse than 57% of composite grades).

MachinabilityPoor28/100
PolishabilityGood55/100

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

Working with TD-Nickel REX

Is TD-Nickel easy to machine?

Machines like tough pure nickel but the ThO₂ abrades tooling — use rigid setups, carbide/ceramic tools, low speed and heavy feed; capture swarf as radioactive-controlled waste.

Can TD-Nickel be welded?

Fusion welding destroys the dispersion and the high-temperature strength at the joint; use solid-state joining (diffusion bonding, brazing, resistance spot) or mechanical fasteners.

Can TD-Nickel be formed, bent or molded?

Made by powder metallurgy (blend/mill, extrude or roll to high strain); sheet is cold formable to moderate radii but strongly anisotropic and prone to splitting across the working direction.

What surface finishes work on TD-Nickel?

Normally left bare for lab use or coated with aluminide/Cr-rich diffusion coatings for oxidising service; can be electropolished, but plating is uncommon.

TD-Nickel 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
ThO2fine dispersoid, ~2 vol%, particle size 20–50 nm1.8 – 2.22
C≤ 0.050.02
Feresidual from powder processing≤ 0.30.1
Oexcluding oxygen bound in ThO₂≤ 0.10.05
Nicommercially pure nickel matrixbalance—

TD-Nickel REX — frequently asked

What is TD-Nickel REX used for?

TD-Nickel REX is typically used for jet-engine hot-section parts (legacy), high-temperature furnace hardware, rocket combustion and nozzle components (legacy), test fixtures for creep and oxidation rigs, heat-shield and radiant panel structures and thermal-processing tooling. In short: first-generation ODS nickel; legacy 1100 °C sheet material; superseded by MA754.

What is the yield strength of TD-Nickel REX?

TD-Nickel REX has a typical yield strength of 270 MPa (39.2 ksi) and a tensile strength of 400 MPa (58 ksi) — weaker than 58% of composite grades. Strength varies by condition: see the 2 listed tempers.

Is TD-Nickel REX easy to machine?

Not especially — machinability is rated poor (28/100, worse than 57% of composite grades). Machines like tough pure nickel but the ThO₂ abrades tooling — use rigid setups, carbide/ceramic tools, low speed and heavy feed; capture swarf as radioactive-controlled waste.

Can TD-Nickel REX be welded?

Fusion welding destroys the dispersion and the high-temperature strength at the joint; use solid-state joining (diffusion bonding, brazing, resistance spot) or mechanical fasteners.

What surface finishes work on TD-Nickel REX?

Normally left bare for lab use or coated with aluminide/Cr-rich diffusion coatings for oxidising service; can be electropolished, but plating is uncommon.

Can TD-Nickel REX be formed, bent or molded?

Made by powder metallurgy (blend/mill, extrude or roll to high strain); sheet is cold formable to moderate radii but strongly anisotropic and prone to splitting across the working direction.

What is the maximum service temperature of TD-Nickel REX?

TD-Nickel REX is rated for continuous use to about 1,250°C (2,282 °F), and briefly to 1,370°C. Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose Materials — ASM International (1990)
  2. ASM Handbook Vol. 21 — Composites (metal-matrix / dispersion-strengthened section) — ASM International (2001)
  3. NASA technical reports on TD-Ni and TD-NiCr sheet for high-temperature structures — NASA Lewis/Langley (1972)
  4. DuPont TD-Nickel / TD-NiCr product literature (historical) — E. I. du Pont de Nemours (1968)
  5. UNS N02120 designation listing — SAE/ASTM Unified Numbering System (2019)

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.