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NiCr22Fe18Mo · UNS N06002 / W86002 (weld)2.4665 · Alloy X / Hastelloy X

Classic gas-turbine combustor alloy — 900 °C-class oxidation resistance

HastelloyNi superalloys
Units
Tensile Rm
655
MPa · ≥ std. min
Yield Rp0.2
240
MPa · ≥ std. min
Elongation A
35
% · ≥ std. min
Service limit
900
°C · indicative max
Density
8.23
g/cm³

Physical properties

Density8.3g/cm³
Modulus E199GPa
Thermal conductivity12W/(m·K)
Thermal expansion14.2×10⁻⁶/K
Specific heat0.42kJ/(kg·K)
Resistivity1.15Ω·mm²/m

Informative values: they vary with composition, condition and test method. Use the governing standard or measured mill data for pressure and heat-transfer calculations.

Chemical composition

Ni 46%Cr 22%Fe 19%Mo 9%Co 1.5%W 0.60%C 0.10%Minor & residual 2.1%

Nominal: mid-range where both limits are given, the cap where only a maximum is, balance takes the remainder. Exact specified ranges below.

ElementName Content %
Main elements7 elements
Ni NickelBal.
Cr Chromium20.5 – 23%
Fe Iron17 – 20%
Mo Molybdenum8 – 10%
Co Cobalt0.5 – 2.5%
W Tungsten0.2 – 1%
C Carbon0.05 – 0.15%
ElementName Content %
Minor & residual4 elements
Si Silicon≤ 1%
Mn Manganese≤ 1%
P Phosphorus≤ 0.04%
S Sulphur≤ 0.03%

Mechanical minima by form

Guaranteed values differ by form, size and delivery condition; quotations confirm the specification, form, size and condition.

FormCondition Rm MPaRp0.2 MPaA ≥ %Other requirements and notes
Bar and forgings
Bar and rodAnnealed ≥ 660 (96 ksi) ≥ 240 (35 ksi) ≥ 35
Plate, sheet and strip
Plate, sheet and stripAnnealed and descaled ≥ 655 (95 ksi) ≥ 240 (35 ksi) ≥ 35
Tube and pipe
Seamless pipe and tubeSolution annealed and descaled ≥ 690 (100 ksi) ≥ 276 (40 ksi) ≥ 35
Welded pipe and tubeSolution annealed ≥ 690 (100 ksi) ≥ 276 (40 ksi) ≥ 35
Fittings and flanges
Fittings (factory-made wrought butt-weld / socket)2150 °F [1177 °C] minimum, rapid air or water quench — — — Tensile properties follow the starting material.
No tension test on the finished fitting unless agreed.
Minimum temperature.
Several forms
Long products ≤160 mm and flat products ≤20 mm (EN 10302, 2.4665)+AT (solution annealed) ≥ 690 ≥ 270 ≥ 30 Flat products under 3 mm: A five points lower.

Creep behaviour

⚠ Scope: these figures apply only to grade 2.4665 (+AT) in EN 10302:2008, as informative guidance; the product standard for this grade specifies no creep data. Use for shortlisting, not for acceptance or design.

Guidance values (MPa) — Mean values of a scatter band. They are neither an acceptance requirement nor a design allowable stress. Figures in parentheses are long-term extrapolations and less reliable than the tested range.

Temp °CCreep strength Rp1.0 (1% plastic strain)Rupture strength Ru
10 000 h100 000 h10 000 h100 000 h
550——360275
600164117254188
65010976175126
700785211982
75051347952
80033205132
85020113219
900115.419.510.6
9505.5211.25.5
10001.9—62.5
12510205010020050010005506006507007508008509009501000Stress MPa (log)Temperature °C10 000 h100 000 h12510205010020050010005506507508501000Stress MPa (log)Temperature °C10 000 h100 000 h12510205010020050010005506006507007508008509009501000Stress MPa (log)Temperature °C10 000 h100 000 h
Logarithmic stress axis. Colour encodes time (1 000 / 10 000 / 100 000 h); solid lines are rupture strength Ru and the dashed line of the same colour is Rp1.0 (1 % plastic elongation). Informative mean values, not acceptance values.

Thermal expansion and elastic modulus

Temperature rangeMean coefficient ×10⁻⁶/K
20–200 °C14.2
20–300 °C14.2
20–400 °C14.2
20–600 °C14.6
20–800 °C15.5
20–1000 °C16.7
051015202003004006008001000×10⁻⁶/KUpper end of interval °CMean expansion α051015202003004006008001000×10⁻⁶/KUpper end of interval °CMean expansion α051015202003004006008001000×10⁻⁶/KUpper end of interval °CMean expansion α
Each point is the mean from 20 °C to that temperature.

Elastic modulus vs temperature

Temp °CE GPa
20199
100196
200190
300184
400178
500171
600164
650161
700157
800149
900141
1000133
120140160180200220201002003004005006007008009001000GPaTemperature °CE120140160180200220202004006008001000GPaTemperature °CE120140160180200220201002003004005006007008009001000GPaTemperature °CE

Grain size

Required by the standard, conditionally — t ≤3.175 mm: ASTM micrograin size No. 3.0 or finer (mean grain dia. 0.127 mm); t >3.175 mm: No. 1.5 or finer (0.214 mm)

Applies to annealed sheet and strip only, banded by thickness; it does not apply to bar — for bar, grain size is specified only for N12160, so Hastelloy X bar carries no grain-size acceptance requirement.

More detail 2

The direction is the reverse of 800H/800HT: here the limit is "No. 3.0 or finer", a floor on the fine side (thin sheet needs fine grain to form), whereas N08810 requires "No. 5 or coarser", a ceiling on the fine side (creep needs coarse grain).

Whenever you see "ASTM grain size number N", check first whether it reads "or finer" or "or coarser".

Where this grade is recommended

Matched in 3 service conditions; ranks and scores computed from the condition-scoring matrix.

Service conditionIndustry TemperatureRankScore
Exhaust & afterburner Aerospace 700 – 950 °C 3 / 8 89
Gas-turbine hot section Power & Nuclear 800 – 950 °C 5 / 10 86
Engine hot section Aerospace 650 – 900 °C 9 / 9 85

Designations & equivalents

UNSN06002 / W86002 (weld)
W.Nr. (Germany)2.4665
EN designationNiCr22Fe18Mo
Trade name(s)Hastelloy X / Nicrofer 6020 hMo
ASTM / AISIB366 / B435 / B572 / B619 / B622 / B626
AMS (SAE aerospace)5390 / 5536 / 5754 / 5798
AWS (welding)A5.14 ERNiCrMo-2
NACE sour serviceISO 15156-3: annealed, no limit on H₂S or temperature; cold-worked ≤40 HRC

Cross-references are common near-equivalents for search and shortlisting; substitution across standards requires clause-by-clause verification. All grades in one cross-reference table →

Applicable standards

11 specifications. Name the standard and its edition on the order.

Guaranteed values and required tests differ between specifications — see Mechanical minima by form for the figures per form.

Frequently asked questions

What is Alloy X · UNS N06002?

Alloy X · UNS N06002 — Ni superalloys. Classic gas-turbine combustor alloy — 900 °C-class oxidation resistance

What is the maximum service temperature of N06002?

Typically about 900 °C; the practical limit depends on media, stress and design life — acceptance per the governing standard.

What is the tensile strength of N06002?

The specified minimum tensile strength is 655 MPa for the main product form. Minima for other forms and sizes are listed under "Mechanical minima by form" on this page.

Which standards cover N06002?

ASTM B366, ASTM B435, ASTM B572, ASTM B619, ASTM B622, ASTM B626, AMS 5390, AMS 5536, AMS 5754, AMS 5798, EN 10302 (creep-resisting steels, nickel and cobalt alloys)

Where is N06002 typically used?

Exhaust & afterburner (Aerospace); Gas-turbine hot section (Power & Nuclear); Engine hot section (Aerospace)

In which forms is N06002 available?

Tube, plate, strip, bar, forgings, wire and other forms — sizes and delivery condition confirmed per order, with EN 10204 3.1 / 3.2 certification.

Same series

Download PDF datasheet

This grade’s datasheet as an A4 PDF — for filing, printing or forwarding to colleagues.

Download PDF datasheet

Supply & enquiry

Tube & pipeφ1 – 219 × 0.25 – 25 mmPlate4.76 – 80 mmBarφ8 – 300 mmWire & filler metalsφ0.01 – 8 mm

For this grade we can supply, against your service conditions:

Or email us: info@kochlin.com