S21906 is a nitrogen-strengthened, high-manganese austenitic chromium-nickel stainless steel (nominally 21% chromium, 6% nickel, 9% manganese — the "21-6-9" composition) that combines high strength with good corrosion resistance and excellent toughness over a very wide temperature range. This datasheet presents the material within the American standard system.
Its room-temperature yield strength is about twice that of the Type 304/321/347 grades, achieved through nitrogen solid-solution strengthening and the high manganese content rather than through cold work or molybdenum. The high manganese and nitrogen stabilise the austenite so effectively that the alloy remains essentially non-magnetic even at cryogenic temperatures or after substantial (up to ~60%) cold work. It offers good high-temperature oxidation resistance in air, resists stress-corrosion cracking in severe marine environments at ambient temperature, and retains high strength and excellent toughness down to cryogenic temperatures (to about -230 °C / -423 °F). Maximum recommended temperature for continuous service is below about 871 °C (1600 °F).
It is readily welded by TIG, MIG and shielded-metal-arc methods (the high nitrogen content can cause outgassing problems in electron-beam welding) and can be hot- and cold-worked, though it is stronger than Type 304 and requires more power. Typical applications include aircraft-engine components, clamps, flanges and hydraulic tubing, chemical-processing and pollution-control equipment, steam and autoclave components, and cryogenic equipment.
Values per manufacturer / reference data, annealed condition.
| Property | Value | Unit |
|---|---|---|
| Density | 7.88 | g/cm³ |
| Melting range | 1390–1440 | °C |
| Maximum continuous service temperature | <871 (1600 °F) | °C |
| Young's modulus (20 °C) | 196 | GPa |
| Thermal conductivity (20 °C) | ~14 | W/m·K |
| Coefficient of thermal expansion (20–100 °C) | ~15.5 | µm/m·°C |
| Electrical resistivity (20 °C) | ~0.71 | µΩ·m |
| Magnetic response | Non-magnetic (stable even after ~60% cold work / cryogenic) | — |
Limiting composition per ASTM A276 / AMS 5656.
| Element | Symbol | Min % | Max % | Role in Alloy |
|---|---|---|---|---|
| Iron | Fe | Balance | — | Base element |
| Chromium | Cr | 19.0 | 21.5 | Passivity; oxidation resistance |
| Manganese | Mn | 8.0 | 10.0 | Austenite stabiliser (replaces some Ni) |
| Nickel | Ni | 5.5 | 7.5 | Austenite stability |
| Nitrogen | N | 0.15 | 0.40 | Solid-solution strengthening; austenite stability |
| Silicon | Si | — | 1.0 | Deoxidiser |
| Carbon | C | — | 0.08 | Controlled |
| Phosphorus | P | — | 0.060 | Residual impurity |
| Sulphur | S | — | 0.030 | Residual impurity |
Nominal: 21Cr-6Ni-9Mn with nitrogen. High manganese and nitrogen stabilise the austenite and provide strength, allowing a reduced nickel content; the closely-related XM-11 variant is a lower-carbon / higher-nitrogen modification.
Typical room-temperature properties, annealed condition.
| Property | Value | Source |
|---|---|---|
| Ultimate tensile strength | ~690–760 MPa | Annealed |
| 0.2% proof strength (yield) | ~380–415 MPa | Annealed |
| Elongation at break | ~45 % | Annealed |
| Hardness | ~90 HRB | Annealed |
| Cryogenic toughness | Excellent | Retained to ~-230 °C |
Room-temperature yield strength is about twice that of Types 304/321/347, from nitrogen and manganese strengthening. The alloy retains high strength and toughness from cryogenic to elevated temperatures. Values are typical; confirm against the mill test certificate.
| Environment | Performance | Notes |
|---|---|---|
| High-temperature oxidation (air) | Good | Continuous service to <871 °C |
| Marine stress-corrosion cracking | Resistant | At ambient temperature |
| General/atmospheric corrosion | Above average | Comparable to / better than 304 |
| Cryogenic toughness | Excellent | To ~-230 °C (-423 °F) |
| Magnetic stability | Excellent | Non-magnetic after cold work / cryogenic |
| Pitting (high chlorides) | Moderate | No molybdenum; below 316 |
| Reducing acids | Limited | As for standard austenitics |
An austenitic stainless steel; it cannot be hardened by heat treatment. High strength comes from nitrogen and manganese; strength can be raised further by cold work.
Solution Anneal approximately 1040–1065 °C (in-process annealing ~1065 °C / 1950 °F), followed by rapid cooling, to dissolve carbides and produce a uniform austenitic structure.
The austenite is highly stable: the alloy remains non-magnetic even after substantial cold work or at cryogenic temperatures. Hot working should be done in the range ~1150–1200 °C (2100–2200 °F).
Readily welded by gas-tungsten-arc, gas-metal-arc and shielded-metal-arc methods, using a matching 21-6-9 filler. The high nitrogen content can cause severe outgassing in electron-beam welding, so that process is generally avoided.
| Process | Applicability | Filler / Consumable |
|---|---|---|
| GTAW / TIG · GMAW / MIG | Good | Matching 21-6-9 |
| SMAW | Good | Matching 21-6-9 electrodes |
| Electron-beam | Avoid | High-N outgassing causes porosity |
No preheat required. Keep joints clean; matching 21-6-9 filler maintains strength and corrosion resistance.
Machining Guidelines
| Parameter | Recommendation |
|---|---|
| Machinability | As for austenitic stainless but stronger; rigid tooling, heavy feeds, slower speeds |
| Tooling | Carbide tools markedly increase removal rates vs HSS |
| Work hardening | High; positive feeds, avoid dwelling |
| Coolant | Ample flood coolant |
Forming Processes
| Process | Notes |
|---|---|
| Hot working | ~1150–1200 °C (2100–2200 °F); stronger than 304 (more power) |
| Cold forming | Same equipment as 304 but more power; in-process anneal ~1065 °C |
| Solution anneal | ~1040–1065 °C, rapid cool |
| Industry | Typical Components | Key Requirements |
|---|---|---|
| Aerospace | Aircraft-engine components, clamps, flanges, hydraulic tubing | High strength; cryogenic toughness |
| Chemical process | Process equipment, vessels | Strength + corrosion resistance |
| Pollution control | Scrubbers, ducting | Corrosion + high-temperature resistance |
| Cryogenic | Low-temperature equipment, vessels | Non-magnetic; toughness to -230 °C |
| Steam / autoclave | Steam and autoclave components | Strength + corrosion resistance |
| Marine | Components in marine environments | SCC resistance |
| Product Form | Standard | Notes |
|---|---|---|
| Bar, wire, rings and extrusions | AMS 5656 · ASTM A276 / A479 | — |
| Sheet, plate and strip | AMS 5595 · ASTM A412 | — |
| Welded tube | AMS 5561 | — |
| Seamless tube | AMS 5562 | — |
| Bar (general) | ASTM A580 · MIL-T-9821 | — |
Nitrogen-strengthened high-manganese 21-6-9 austenitic stainless steel. UNS S21900 / S21904; AMS 5656 / 5595 / 5561 / 5562; ASTM A276 / A412 / A580. Tradename: Nitronic 40 (registered trademark of Cleveland-Cliffs).
| UNS | Nominal | Yield (approx) | Best Used For |
|---|---|---|---|
| S21906 | 21Cr-6Ni-9Mn-N | ~55 ksi | Non-mag high strength; aircraft, cryogenic |
| S20910 | 22Cr-13Ni-5Mn-Mo-N | ~60 ksi | Higher corrosion + strength (with Mo) |
| S30400 | 18Cr-8Ni | ~30 ksi | General stainless (reference) |
| S31600 | 17Cr-12Ni-2Mo | ~30 ksi | General Mo stainless (reference) |
| S21800 | 17Cr-8Ni-8Mn-4Si-N | ~55 ksi | Galling/wear + high strength |
Next:Alloy 40