Density |
N/A 0.274 lb/in³ |
Electrical Resistivity |
N/A 589 ohm/cir-mil-ft |
Thermal Expansion Coefficient at 68 to 212 Degree Fahrenheit (ºF) |
N/A 8.8 x 10-6 in/in/ºF |
Mechanical Type |
N/A Annealed |
Tensile Strength |
N/A 105 ksi |
Yield Strength |
N/A 52 ksi |
Elongation |
N/A 64 % |
Hardness |
N/A B95 |
Nickel (Ni) |
N/A 8.5 |
Iron (Fe) |
N/A 63 |
Chromium (Cr) |
N/A 17 |
Manganese (Mn) |
N/A 8 |
Nitrogen (N) |
N/A 0.14 |
Silicon (Si) |
N/A 4 |
Maximum Carbon (C) |
N/A 0.08 |
General Resistance |
N/A Temperature Oxidation Wear Galling Corrosion |
Unified Numbering System (UNS) |
N/A S21800 |
Sheet/Plate USA |
N/A A240 |
Bar/Rod USA |
N/A A193 A194 A276 A479 AMS 5848 |
Forging USA |
N/A A193 A194 A276 A479 AMS 5848 |
Weld Wire |
N/A A5.9 ER218 |
Speed Surface |
N/A Annealed: 40 ft/mmGrade A: 38 ft/mmGrade B: 36 ft/mmGrade C: 32 ft/mmGrade D: 28 ft/mmGrade E: 25 ft/mm |
Speed Percent (%) of B1112 |
N/A Annealed: 24 Grade A: 23 Grade B: 22 Grade C: 19 Grade D: 17 Grade E: 15 |
Note |
N/A These machinability ratios must be recognized as approximate values. They are a reasonable guide to relative tool life and lower required for cutting. It is obvious, however, that variables of speed, cutting oil, feed and depth of cut will significantly affect these ratios. |
N/A
The alloys described here work harden rapidly during machining and require more power to cut than do the plain carbon steels. The metal is 'gummy', with chips that tend to be stringy and tough. Machine tools should be rigid and used to no more than 75% of their rated capacity. Both work piece and tool should be held rigidly; tool overhang should be minimized. Rigidity is particularly important when machining titanium, as titanium has a much lower modulus of elasticity than either steel or nickel alloys. Slender work pieces of titanium tend to deflect under tool pressures causing chatter, tool rubbing and tolerance problems. |
N/A
Corrosion Properties |
N/A
|
Additional Information |
N/A
Valves stems, seats, and trim; fastening systems, screening, pins, bushings, roller bearings, pump shafts and rings. Food handling, medical, automotive, aerospace and nuclear. Austenitic Stainless Nitronic 60 is truly an all purpose metal. This fully austenitic alloy was originally designed as a wear alloy, and subsequently has good high temperature properties for temperatures around 1800 ºF. The oxidation resistance of Nitronic 60 is similar to Type 309 S.S., and far superior to Type 304S.S. The additions of Silicon and Manganese have given this alloy a matrix to inhibit wear, galling, and fretting even in the annealed condition. Higher strengths are attainable through cold working the material and are still fully austenitic after severe cold-working. This working does not enhance the anti-galling properties as is normal for carbon steels and some stainless steels. The benefit to the cold or hot work put into the material is added strength and hardness, and the wear resistance does not decrease noticeably. Chromium and Nickel additions give it comparable corrosion to 304 and 316 stainless steels, while having approximately twice the yield strength. The high mechanical strength in annealed parts permits use of reduced cross sections for weight, and cost reductions through the use of thinner stock. Several data sheets are available on the wear compatibility of this alloy with dissimilar couples, as well as self-mated coupled results. If you're galling problem occurs at less than 1500 ºF, then you should think about switching to this alloy. Nitronic 60 has a better cost advantage than any other alloy available. Other materials require an additional amount of heat treating to raise their hardness, where Nitronic 60 is excellent in the annealed condition. |