Austenitic

Austenitic

S21900

Overview

S21900 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.

1. Physical Properties

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)

2. Chemical Composition (wt %)

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.

3. Mechanical Properties

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.

4. Corrosion and High-Temperature Resistance

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

5. Heat Treatment

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).

6. Weldability and Joining

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.

7. Machinability and Fabrication

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

8. Applications

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

9. Available Product Forms and Standards

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).

10. Comparison with Related Alloys (UNS System)

UNS Nominal Yield (approx) Best Used For
S21900 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


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