Steel
Steel AM 100
Annealing Procedure
For optimum softening for machining, normalize at 1650 F and overage anneal at 1250 F for 16 hours. This should result in a Rc 40 maximum hardness.
Applications
AM 100 has been successfully employed in jet engine shafts, a variety of ordnance and ballistic components, as well as in fasteners.
Heat Treatability
Normalize by heating to 1650 F and hold for 1 hour, then air cool. For optimum softening for machining, normalize at 1650 F and overage anneal at 1250 F for 16 hours.
Machinability
Machining this alloy is considered somewhat more difficult than machining 4340 at Rc 38. Carbide tooling is recommended at 280 to 350 SFM.
Principle Design Features
This is an alloy designed for high strength, fracture toughness and hardness.
Known Forms
Angle
Billet
Cee
Channel
Coil
Disc
Drill Rod
Flat Bar
H-Beam
Half Round
Hexagon Bar
Hollow Bar
Octagon Bar
Piling
Pipe
Plate
Precision Ground Bar
Rectangle Tube
Ring
Rod
Round Bar
Round Tube
Sheet
Square Bar
Square Tube
Standard Beam
Strip
Tee
Treadplate
Wide Beam
Zee
Additional Data
Specifications
K92580Chemical Elements
| Carbon | 0.23 nom |
| Chromium | 3.1 nom |
| Cobalt | 13.4 nom |
| Iron | Balance |
| Molybdenum | 1.2 nom |
| Nickel | 11.1 nom |
Physical Properties
Density: 0.285lb/in³