Inconel MA758 belongs to a small, specialized family of oxide-dispersion-strengthened (ODS) superalloys produced by mechanical alloying rather than conventional melting and casting. In the mechanical alloying process, elemental and master-alloy powders are milled together with a fine yttrium oxide (Y2O3) powder under high-energy conditions until the yttria particles are driven into true solid solution within each metal powder particle. The powder is then consolidated and hot-worked, leaving an extremely fine, uniform dispersion of oxide particles locked inside the nickel-chromium matrix. Unlike conventional superalloys that get their high-temperature strength from precipitated intermetallic phases that coarsen and dissolve as temperature rises, MA758 draws its strength from these thermally stable oxide particles, which physically block dislocation movement and stay put even near the alloy's melting point.
That gives MA758 a strength advantage at very high service temperatures that few conventionally processed alloys can match, alongside strong resistance to oxidizing atmospheres from its roughly 30% chromium content. It sits in the same processing family as the better-known MA6000, but with a simpler, solid-solution-type matrix rather than a gamma-prime-hardened one. In practice, MA758 shows up in gas turbine components, combustion hardware, and other parts that spend long periods at temperatures where conventional nickel alloys would start to lose their grip.
| Standard | Designation |
|---|---|
| UNS | N07758 |
| Trade Name | Inconel MA758 (Special Metals) |
MA758 is a proprietary mechanically alloyed grade. A widely published DIN/Werkstoffnummer equivalent could not be independently verified, so it has been omitted rather than guessed.
| Element | Content |
|---|---|
| Nickel (Ni) | Balance (~67%) |
| Chromium (Cr) | ~30.0% |
| Yttrium Oxide (Y2O3) | ~0.6% (dispersoid) |
| Titanium (Ti) | ~0.5% |
| Aluminum (Al) | ~0.3% |
| Iron (Fe) | 1.0% max |
| Carbon (C) | 0.05% max |
The yttrium oxide content is a dispersed second-phase particle, not a dissolved alloying element — it is what gives MA758 its oxide-dispersion-strengthened behavior.
MA758 carries every classic nickel-superalloy machining challenge and then adds one more on top. Like other high-nickel, high-chromium alloys, it has low thermal conductivity, so cutting heat concentrates at the tool edge instead of flowing into the chip, and it work-hardens quickly under light or rubbing cuts, which punishes tools that dwell or hesitate. Nickel's chemical affinity for the tool material also promotes galling and built-up edge, especially at lower cutting speeds where temperatures aren't high enough to keep the interface clean.
What sets MA758 apart is the yttria dispersoid itself. Those sub-micron oxide particles are what make the alloy strong at temperature, but they are also intensely abrasive — closer in behavior to a fine ceramic filler than a metallic constituent. Every particle the cutting edge encounters acts like a tiny abrasive grain grinding against the flank and rake faces, which drives flank wear rates well above what you'd see in a solid-solution or even a precipitation-hardened nickel alloy of similar hardness. This is why MA758 and its ODS relatives are typically cut at noticeably lower speeds than conventional Inconel or Nimonic grades of comparable strength.
In practice, that means erring conservative on speed, keeping feeds firm enough to stay under the work-hardened layer from the previous pass, and treating tool life — not surface finish — as the limiting factor. A rigid setup, sharp edges, and a wear-resistant coating matched to abrasive wear (rather than just heat resistance) make the biggest difference here.
| Operation | Vc (m/min) | Vc (SFM) |
|---|---|---|
| Turning | 15 – 35 | 50 – 115 |
| Milling | 12 – 25 | 40 – 80 |
| Parting | 10 – 20 | 35 – 65 |
| Grooving | 12 – 25 | 40 – 80 |
These are conservative starting points reflecting the abrasive oxide dispersion in MA758 — well below typical wrought nickel-superalloy speeds. Assumes a well-matched insert grade, rigid clamping, short overhang, and nominal hardness. Adjust down further for interrupted cuts or poor rigidity.
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM524 | CVD | S05 – S10 |
| FM2533 | CVD | S15 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM2543 | CVD | S20 |
| FM2553 | CVD | S30 |
| FM2533 | CVD | S10 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM125 | PVD | S15 – S35 |
Ready to cut MA758? Shop FM Carbide inserts matched to this ODS superalloy's turning, parting, grooving, and milling requirements.
Shop Turning & Grooving Inserts Shop Milling Inserts| 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" |