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300m Alloy Steel

Typical Applications

Aircraft Landing Gear

Driveshafts

High Strength bolts

Gears

AMS 6257, AMS 6417, AMS 6419 Suppliers & Stockholders

Dynamic Metals is a specialist supplier and stockholder of 300M alloy steel, supplying aerospace and defence industries with certified material to AMS 6257, AMS 6417, AMS 6419 and BS S155 since 1997. No minimum order quantities.

300M is a low alloy, vacuum melted, highly strength steel that is an improved version of the AISI 4340 steel, where the percentage of silicon, vanadium and carbon and molybdenum are increased. In accordance with AMS 6257, AMS 6417 and AMS 6419, 300M provides tensile strength up to 1900-2100 MPa as a result of final heat treatment – the highest tensile strength of through hardening alloy steel available.

The main difference between 300M and ordinary 4340 is a high strength coupled with the properties of toughness and fatigue resistance. Silicon content increases strength and prevents steel from softening under tempering process, whereas the increase in the content of vanadium leads to finer grain structure and prevents grain growth during the heat treatment. The combination of these two results in significantly increased fracture toughness of 300M as compared to other steels with similar strength values.

300M is a vacuum melted steel used in aerospace industry. The manufacturing process helps to reduce the number of non-metallic inclusions and to provide the purity of material. It is a through hardening alloy with uniform properties through thicknesses needed for landing gear. Austenitizing temperature is about 871°С; further oil quenching and double tempering at 315°С are performed.

Main applications of 300M include aircraft landing gear – the dominating material in this sphere for decades now, as well as rocket motor casings, driveshafts, high strength fasteners and structural airframe parts.

Technical specification

Related Specifications

AMS 6257
AMS 6417
AMS 6419
BS S155
BMS 7-26
MTL 1201
MIL S 8844

Specific Gravity

7.83 g/cm3

Chemical Composition (WT %)

 
Min  
Max  
C  
0.39  
0.44  
Si  
1.5  
1.8  
Mn  
0.6  
0.9  
P  
-  
0.015  
S  
-  
0.015  
S+P  
-  
0.025  
Cr  
0.7  
0.95  
Mo  
0.3  
0.45  
Ni  
1.65  
2  
V  
0.05  
0.10  

Typical Mechanical Properties

 
 
 
Longitudinal  
Transverse  
0.2% Proof Stress  
MPA  
Min  
1550  
1550  
Tensile Strength  
MPA  
Min  
1900  
1900  
Tensile Strength  
MPA  
Max  
2100  
2100  
Elongation  
%  
Min  
8  
5  
Reduction of area  
%  
Min  
30  
20  

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