Maraging T200 belongs to the cobalt-free branch of the 18% nickel maraging steel family, developed as an alternative to the cobalt-bearing C-series grades for buyers who wanted to avoid cobalt's price volatility and supply constraints without giving up the maraging concept. The name still describes the same underlying process — "martensite" plus "aging": on cooling from solution-annealing temperature, the very low-carbon nickel-molybdenum-titanium chemistry forms a soft, easily worked martensite, and a subsequent aging treatment at moderate temperature precipitates fine intermetallic compounds through that structure to build strength.
Without cobalt's contribution to the aging response, T-series grades rely on higher titanium content to reach comparable strength levels to their C-series counterparts, and they generally trade a bit of toughness for that simplification in alloy design. T200 is used in the same general categories of application as the cobalt-bearing grades — aerospace structural components, high-performance tooling, and precision shafting — particularly where cost stability or cobalt availability makes the cobalt-free chemistry the more practical choice.
No independently verifiable AISI/SAE, DIN, or UNS cross-reference numbers were available for this specific cobalt-free maraging grade in the source data. Confirm designation cross-references against mill certification for critical applications.
| Element | Content (typical) |
|---|---|
| Nickel (Ni) | 18.5% |
| Molybdenum (Mo) | 3% |
| Titanium (Ti) | 1.4% |
| Aluminum (Al) | 0.1% |
| Carbon (C) | 0.02% max |
| Manganese (Mn) | 0.05% max |
| Silicon (Si) | 0.03% max |
| Phosphorus (P) | 0.005% max |
| Sulfur (S) | 0.005% max |
| Iron (Fe) | Balance |
Typical/nominal values for this cobalt-free grade. Note this grade is not standardized as consistently as the cobalt-bearing C-series, so confirm exact chemistry against mill certification for critical applications.
Like every alloy in the maraging family, T200's machinability depends heavily on its heat-treatment condition. In the solution-annealed (unaged) state, the low-carbon martensite is soft and ductile, machining comparably to a mild-to-moderate alloy steel with reasonable cutting forces and predictable tool wear. This is the condition in which the bulk of rough and semi-finish machining is normally performed, before the part is aged to its final strength.
Once aged, this grade reaches roughly 50.5 HRC, and machining becomes noticeably more demanding — higher cutting forces, faster tool wear, and a general shift toward grinding or light precision cuts for any post-aging shaping. Because the strengthening in maraging steel comes from fine, coherent intermetallic precipitates rather than a coarse carbide network, aged T200 doesn't behave quite like an equally hard conventional tool steel, but the process window still narrows considerably compared with the annealed condition. The cutting parameters below apply to the solution-annealed, pre-aging condition.
| Operation | Vc (m/min) | Vc (SFM) |
|---|---|---|
| Turning | 90 – 130 | 295 – 425 |
| Milling | 55 – 80 | 180 – 260 |
| Parting | 45 – 65 | 150 – 215 |
| Grooving | 50 – 70 | 165 – 230 |
| Drilling | 35 – 55 | 115 – 180 |
Values apply to the solution-annealed (unaged) condition. Reduce speeds substantially and favor tougher, wear-resistant grades for material machined after aging (~50.5 HRC).
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM2543 | CVD | P20 |
| FM324 | PVD | P20 – P30 |
| FM2553 | CVD | P30 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM324 | PVD | P20 – P30 |
| FM2553 | CVD | P30 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM125 | PVD | P15 – P35 |
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