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Type 321 is an "18-8" chromium-nickel stainless steel modified by the addition of titanium to overcome the danger of intergranular corrosion, common to other austenitic stainless steels during or after exposure to temperatures of 800°F. This type is non-magnetic in the annealed condition and not hardenable by heat treatement. It is manufactured by the electric furnace process to meet the rigid requirements of the aircraft industry
| Typical Mechanical Properties | ||
|---|---|---|
| Annealed | Normalized | |
| Tensile Strength (ksi) | 85 max | 90-95 min |
| Yield Point (ksi) | - | 70-75 |
| Elongation (% in 2") | - | 18-Aug |
| Typical Chemical Analysis | |
|---|---|
| C | .08 max |
| Mn | 2.00 max |
| P | .040 max |
| S | .030 max |
| Si | 1.00 max |
| Cr | 17.0 - 19.0 |
| Ni | 9.00 - 12.00 |
| Ti | 6xC - .70 |
| Cu | .75 max |
| Mo | .75 max |
Please note, this information is to be used as a guide only, for more specific information please
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