Kg & pieces - No decimal places. Thanks to its high chromium content, this steel resists oxidation and corrosion even under aggressive conditions such as intergranular corrosion. Its reinforcement with manganese and nitrogen increases the strength and stability of the austenite and gives it excellent toughness, which it retains down to temperatures close to those of liquid helium (-269 °C or -516 °F). The 21-6-9 alloy does not respond to heat treatments for hardening by quenching, tempering, or aging, unlike martensitic steels. On one hand, it does not contain enough aluminum, titanium, or copper to allow for age hardening. On the other, its austenite is too stable at low temperatures for quenching or tempering to be effective. However, cold working to increase hardness is possible—or hot working to improve ductility—without degrading the material. 21-6-9 stainless steel should be hot worked in a temperature range between 927 °C and 1204 °C (1700–2200 °F). Maintaining a controlled temperature is essential to avoid damaging the material’s microstructure. Cold working includes rolling, drawing, and stamping at room temperature. Due to its high work hardening rate, 21-6-9 requires higher forming forces than other austenitic stainless steels (such as 302, 304, and 316). An intermediate anneal is necessary to reduce hardness and facilitate further cold working. This process (cold work → anneal → further cold work) significantly increases its yield strength. When hardened (work hardened), 21-6-9 has a yield strength of at least 827 MPa, ensuring durability under heavy loads. Its tensile strength can reach 1117 MPa. Its elongation capability is at least 35 % in the annealed state, and it maintains at least 20 % elongation when hardened. This alloy remains non-magnetic even after severe cold working, an important characteristic of Nitronic grades (unlike 301/304 steels, which can become slightly magnetic after work hardening due to martensite formation). The austenite in 21-6-9 is very stable. Because of its high work hardening rate, 21-6-9 is more difficult to machine than most austenitic stainless steels. Similar to type 316, it is recommended to use slow cutting speeds, positive feeds, and ample cutting fluids. It offers good formability and handling in the annealed condition. However, its high yield strength and work hardening rate require greater forces during forming than other steels like 304L. Techniques such as bending, drawing, and stretching can be applied, but an intermediate anneal may be necessary to prevent cracking and ensure uniform deformation. 21-6-9 is considered to have good weldability. Several welding methods can be successfully applied: Oxy-acetylene welding should be avoided, as it risks carbon buildup that would compromise the material’s properties. In addition to the aerospace industry, the 21-6-9 alloy is also used for: The variations in its chemical composition for aerospace. RECTANGULAR BAR, ROUND BAR, PROFILE, SHEET SQUARE BAR, RECTANGULAR BAR, ROUND BAR, SHEET SHEET MOTHER COIL, COIL, SHEET SHEET RECTANGULAR BAR, ROUND BAR, SHEET, ROUND TUBE SQUARE BAR, RECTANGULAR BAR, ROUND BAR, SHEET ROUND BAR SHEET ROUND BAR ROUND BAR ROUND BAR ROUND BAR ROUND BAR RECTANGULAR BAR ROUND BAR, COIL, SHEET (THICKNESS > 6MM) SQUARE BAR SQUARE BAR, RECTANGULAR BAR, ROUND BAR, COIL, WIRE, SHEET ROUND BAR ROUND BAR RECTANGULAR BAR, ROUND BAR ROUND BAR ROUND BAR ROUND BAR ROUND BAR ROUND BAR ROUND BAR, SHEET ROUND BAR ROUND BAR SHEET ROUND BAR SHEET ROUND BAR, SHEET ROUND BAR RECTANGULAR BAR, ROUND BAR, COIL, WIRE, PROFILE, SHEET, PERFORATED SHEET, PVC SHEET, ROUND TUBE ROUND BAR, SHEET SQUARE BAR, RECTANGULAR BAR, ROUND BAR, COIL, SHEET, ROUND TUBE The most remarkable properties of this stainless steel alloy The practical applications of this stainless steel in aircraft construction. A key application area for 21-6-9, used in liquid-fueled rockets. 21-6-9 is used in compressor casings or engine exhaust systems for its good fatigue and corrosion resistance, as well as its formability. Another major application of 21-6-9 is in the aircraft's hydraulic system, including fittings, for example, and components of the landing gear. How it is used in various industries.General Introduction to 21-6-9
Hot Working, Cold Working
Serve while it's hot.Mechanical and Chemical Properties
Machinability, Formability
Weldability
Industrial applications
Chemical composition of 21-09-06
% C
CarbonCr
ChromiumCu
CopperMn
ManganeseMo
MolybdenumN
NitrogenNi
NickelP
PhosphorusS
SulfurSi
Silicon Min. <0.00 19.00 <0.00 8.00 <0.00 0.15 5.50 <0.00 <0.00 <0.00 Max. 0.04 21.50 0.75 10.00 0.75 0.40 7.50 0.03 0.03 1.00 Related stainless steel alloys
15-5PH, 1.4545, X5CrNiCu15-5, EZ5CNU15.15
17-4PH, 1.4548, UNS S17400, AMS 5643, AMS 5622, S17400
17-7PH, S17700, 1.4568, AISI 631, X7CrNiAl17-7
AISI 301, X12CrNi17-07, Z12CN17-07
AISI 302
AISI 347, X6CrNiNb18-10, Z6CNNb18-10
AISI 431, APX, X15CrNi17-03, Z15CN17-03
AISI 446
CALE PELABLE
CUSTOM 465, MLX17, X1CrNiMoAlTi12-11
EZ100CD17
EZ12CNDV12
EZ15CN17-03
EZ1CNDAT12-09, MARVALX12, X1CrNiMoAlTi12-9
EZ2NKD18-8-5, MARAGING 250, X2NiCoMo18-8-5
EZ3NCT25, X3NiCrTi25
EZ6CND16-05-01
EZ6NCT25, A286, X6NiCrTi25
EZ8CND17-04
GD223, X50NiMnCr12, Z50NMC12
PH13-8Mo, X3CrNiMoAl13-08-02, Z3CND13-08
S130
S143
S143D
S144
S145
X12C13, X12Cr13, AISI 410, 1.4006, Z10C13
X30Cr13, Z30C13
X6Cr17
X750
Z100CD17
Z12CN13
Z12CNDV12, JETHETE M152, X12CrNiMoV12
Z25CNWS22
Z2CN18-10, AISI 304L, X1CrNi18-10
Z6CND16-05-01, APX4, Z8CND17-04, X4CrNiMo16-5-1
Z6CNT18-10, AISI 321, X6CrNiTi18-10, X6CNT18-10
Key properties
How 21-09-06 is used in aerospace
Cryogenic tanks and lines
Casings and housings
Hydraulic tubing
Optimizing the use of 21-09-06 : treatments, regulations, and options.
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21-09-06 stainless steel