Technical Reference Library
Nimonic PE13
UNS N06002
Wnr. 2.4665
Material Overview
Nimonic PE13 shares its base chemistry with the alloy sold elsewhere as Hastelloy X or Inconel HX (UNS N06002) — a nickel-chromium-iron-molybdenum superalloy built around roughly 20.5-23% chromium, 17-20% iron, and 8-10% molybdenum on a nickel base, with a small tungsten addition. Unlike the age-hardened Nimonic grades, this chemistry gets its properties from solid-solution strengthening rather than precipitation hardening, which trades outright strength for exceptional stability and oxidation resistance at very high temperatures.
That combination is exactly what combustor and afterburner hardware needs: this chemistry resists oxidation up to roughly 1200°C (2200°F), holds its strength through extended high-temperature exposure, and forms and welds more readily than most precipitation-hardened superalloys since there's no aging response to disturb during fabrication. It shows up routinely in combustion chambers, transition ducts, afterburner components, and other gas-turbine hot-section hardware, as well as in industrial furnace fixtures and other equipment that needs to survive sustained high-temperature service without the machining difficulty of a fully age-hardened alloy.
International Designation Equivalents
| Standard |
Designation |
| UNS |
N06002 |
| Wnr. (Werkstoffnummer) |
2.4665 |
| Equivalent Chemistry |
Hastelloy X / Inconel HX family |
Chemical Composition
| Element |
Content |
| Nickel (Ni) |
Balance (~47%) |
| Chromium (Cr) |
20.5 – 23.0% |
| Iron (Fe) |
17.0 – 20.0% |
| Molybdenum (Mo) |
8.0 – 10.0% |
| Cobalt (Co) |
0.5 – 2.5% |
| Tungsten (W) |
0.2 – 1.0% |
| Manganese (Mn) |
1.0% max |
| Silicon (Si) |
1.0% max |
| Carbon (C) |
0.05 – 0.15% |
Machinability Explained
This chemistry is demanding to machine, though somewhat less so than the fully age-hardened Nimonic grades, since it relies on solid-solution strengthening rather than gamma-prime precipitates for its high-temperature capability. Low thermal conductivity is still the dominant factor: heat generated at the cutting edge has nowhere to go but into the tool, so temperatures build quickly even at modest cutting speeds. The high chromium and molybdenum content also keeps hot hardness elevated, meaning the material doesn't soften helpfully the way carbon steel does as the cut heats up.
Work-hardening remains a real concern — light or hesitant cuts burnish the surface and leave a hardened layer that resists the next pass, so feed rates need to stay heavy enough to consistently cut beneath it. The alloy also tends toward galling and built-up edge rather than clean chip shear, which accelerates flank wear and can tear the surface finish if tooling isn't matched to the job. Rigid, low-deflection setups, sharp positive-rake geometry to minimize cutting forces, and coatings selected for hot hardness and adhesion resistance all make a measurable difference in tool life on this chemistry.
Recommended Cutting Speeds
| Operation |
Vc (m/min) |
Vc (SFM) |
| Turning |
55 – 75 |
180 – 245 |
| Milling |
40 – 55 |
130 – 180 |
| Parting |
35 – 50 |
115 – 165 |
| Grooving |
45 – 65 |
150 – 210 |
| Drilling |
45 – 65 |
150 – 210 |
Values assume favorable cutting conditions: a well-matched insert grade, rigid tool and workpiece clamping, good-quality raw material, short tool overhang, and nominal material hardness. Adjust down for interrupted cuts, poor rigidity, or harder-than-nominal stock.
Recommended FM Carbide Grades by Operation
Turning
| Grade |
Coating |
ISO Application Range |
| FM524 |
CVD |
S05 – S10 |
| FM2533 |
CVD |
S15 |
Parting / Grooving
| Grade |
Coating |
ISO Application Range |
| FM2543 |
CVD |
S20 |
| FM2553 |
CVD |
S30 |
| FM2533 |
CVD |
S10 |
Milling
| Grade |
Coating |
ISO Application Range |
| FM125 |
PVD |
S15 – S35 |
Recommended Insert Cutting-Edge Geometry
| Parameter |
Value |
| Honing Size |
0.02 – 0.05 mm / 0.001 – 0.002" |
| Rake Angle |
13° – 18° |
| Land Angle |
Neutral |
| Land Width |
0.10 – 0.20 mm / 0.004 – 0.008" |
| Ground Insert |
Recommended |