Steel 300M

Aging Procedure

Not applicable to this alloy.

Annealing Procedure

Anneal at 1550 F and slow furnace cool at a rate of less than 50 F per hour down to 600 F. From there it may be air cooled.

Applications

Applications for 300M steel are those that require strength in the 290 - 300 ksi range, such as aircraft landing gear, high strength bolts and airframe parts.

Cold Workability

In the annealed or normalized condition the alloy has good ductility and can be readily cold worked by conventional methods.

Forgeability

No data. The alloy is forgeable - contact the supplier for details.

Formability

Formability by conventional methods is good in the annealed condition. The alloy behaves much like AISI 4340 steel.

Hardening Procedure

300M hardens from cold working and by heat treatment. See "Heat Treatment" and "Tempering".

Heat Treatability

300M must be normalized at 1700 F before hardening. After the normalizing treatment the alloy is hardened by heating to 1600 F and oil quenching. Tempering is then done last.

Hot Workability

No data. Heat input can cause this alloy to air harden. Contact the alloy supplier for information as to the advisability of hot working.

Machinability

Machining is best accomplished with the alloy in the normalized or normalized and tempered condition. Final machining to finish tolerances is done by grinding with care due the hardness of the heat treated alloy (Rockwell C 55). It is important to do a stress relief anneal at 550 F after finish grinding.

Other Comments

300M may be joined by Nicer brazing, copper brazing and silver brazing.

Principle Design Features

300M is a low alloy, vacuum melted, steel of very high strength. Essentially it is a modified AISI 4340 steel with silicon, vanadium and slightly greater carbon and molybdenum content than 4340. 300M has a very good combination of strength (280 to 305 ksi), toughness, fatigue strength and good ductility. It is a through hardening alloy.

Tempering Procedure

Temper at 600 F to give a nominal 300 ksi strength.

Weldability

300M can be welded by fusion methods or by flash resistance welding. Approved procedures must be used for fusion welding, including pre and post-heating practice, because the alloy will air harden due to heat input from welding. Following welding it is essential to re-normalize or re-normalize and temper prior to the final hardening heat treatment.

Known Forms

Angle

Angle

Billet

Billet

Cee

Cee

Channel

Channel

Coil

Coil

Disc

Disc

Drill Rod

Drill Rod

Flat Bar

Flat Bar

H-Beam

H-Beam

Half Round

Half Round

Hexagon Bar

Hexagon Bar

Hollow Bar

Hollow Bar

Octagon Bar

Octagon Bar

Piling

Piling

Pipe

Pipe

Plate

Plate

Precision Ground Bar

Precision Ground Bar

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Square Tube

Square Tube

Standard Beam

Standard Beam

Strip

Strip

Tee

Tee

Treadplate

Treadplate

Wide Beam

Wide Beam

Zee

Zee

Additional Data

Specifications

6417,6419,A579 (32),A646 (300M-8),S-8844 (3),S-8844 Class 2,K44220

Chemical Elements

Carbon0.38 - 0.46
Chromium0.7 - 0.95
IronBalance
Manganese0.6 - 0.9
Molybdenum0.3 - 0.65
Nickel1.65 - 2
Phosphorus0.01 max
Silicon1.45 - 1.8
Sulphur0.01 max
Vanadium0.05 nom

Physical Properties

Density: 0.283lb/in³Density

Melting Point: 2590°FMelting Point

Specific Gravity: 7.83Specific Gravity

Specific Heat: 0.116BTU/lb·°FSpecific Heat

Mechanical Properties

Modulus of Elasticity – Tension: 29MSIModulus of Elasticity – Tension

Thermal Conductivity: 1.75BTU/hr·ft·°FThermal Conductivity

Thermal Expansion: 6.6µin/in·°FThermal Expansion