MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Rulon Bearings

(Viewing data as-entered. Click here to return)
QuesTek® Innovations Ferrium® S53® Corrosion Resistant High Strength Steel for Aerospace Structural Applications
Categories: Metal; Ferrous Metal; Alloy Steel

Material Notes: Description: Ferrium® S53® is a corrosion resistant ultra high-strength steel for structural aerospace applications. Ferrium® S53® was designed to provide mechanical properties equal to, or better than, conventional ultrahigh-strength steels such as 300M and SAE 4340 with the added benefit of general corrosion resistance. This eliminates the need for cadmium coating processes, which are environmentally unfriendly and require subsequent hydrogen bake-out operations in order to avoid hydrogen embrittlement. Ferrium® S53® has a greatly improved resistance to stress-corrosion cracking (SCC) over 300M and SAE 4340. Ferrium® S53® utilizes an efficient M2C strengthening dispersion precipitated through tempering while avoiding other carbides. This maximizes strength, wear resistance, and toughness; resulting in a unique combination of mechanical properties for a corrosion resistant steel. Ferrium® S53® uses a stable passive oxide film for optimum corrosion resistance. It also has high hardenability, permitting less severe quench conditions for a given section size and resulting in less distortion during heat treatment. S53® should be considered for use in applications requiring high strength with good fracture toughness, corrosion resistance and high resistance to stress-corrosion cracking (per ASTM F1624). S53® is supplied in a normalized and annealed condition. The dimensional change upon hardening from the annealed condition is approximately 0.003 in./in.

Typical Applications: Aircraft landing gears, flap tracks, actuators, fasteners and other structural applications.

Workability:
Fording: Forge at 2050°F (1121°C) followed by an air cool, normalize, subzero treatment and anneal.
Machinaility: Annealed Ferrium® S53® has machinabilty similar to 300M at 35 HRC.
Passivation: Passivation in a 50% nitric acid solutions recommended for maximum corrosion resistance per AMS 2700B, Method 1

Heat Treatment:
Solution Treatment: 1985°F(1085°C) 1 hour and oil quench or equivalent, water quenching is not recommended. Soak time must be closely monitored, load couples are recommended.
Sub Zero Treatment: Following the solution treatment, -100°F(-73°C), 1 hour and air warm.
Tempering: 934°F (501°C), 3 hours and oil quench or equivalent followed by -100°F(-73°C), 1 hour and air warm then a second temper at 900°F(482°C) 12 hours and air cool.

    Other Key Properties
  • Corrosion resistance has been measured using a variety of test methods. General corrosion resistance of S53® is similar to 440C.
  • Fatigue testing at a number of R values and stress levels has shown equivalent performance to typical 300M values.
  • S53® yields a Class A Weld. Welding studies have shown minimal impact on mechanical properties.
Product Forms: Ferrium® S53® may be manufactured in typical ingot, bar, and billet forms. Sheet and plate also available upon request.

Ferrium is designed by Questek Innovations, LLC. and is manufactured by Latrobe Specialty Steel under license.

Key Words: UNS S10500, AMS 5922
Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Density 498 lb/ft³
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 54typical
Tensile Strength at Break >= 280000 psi
Tensile Strength, Ultimate 288 ksiTypical
Tensile Strength, Yield >= 213 ksi
@Strain 0.2 %
 225 ksi
@Strain 0.2 %
Elongation at Break >= 11 %
 15 %
Reduction of Area 55 %Transverse
 57 %Flow
Tensile Modulus 204 GPa
Compressive Yield Strength 260000 psi
Ultimate Bearing Strength 451000 psie/D = 1.5
 589000 psie/D = 2.0
Bearing Yield Strength 370000 psie/D = 1.5
 452000 psie/D = 2.0
Fracture Toughness 65.0 ksi-in½
Shear Strength 181000 psi
Charpy Impact 18.0 ft-lbV-notch
 
Thermal PropertiesOriginal ValueComments
CTE, linear 10.53 µm/m-°C
@Temperature 24.0 - 104 °C
 10.59 µm/m-°C
@Temperature 24.0 - 204 °C
 10.79 µm/m-°C
@Temperature 24.0 - 316 °C
 11.02 µm/m-°C
@Temperature 24.0 - 427 °C
 11.13 µm/m-°C
@Temperature 24.0 - 593 °C
 11.18 µm/m-°C
@Temperature 24.0 - 538 °C
Specific Heat Capacity 0.108 BTU/lb-°F
@Temperature 22.8 °C
 0.120 BTU/lb-°F
@Temperature 200 °C
 0.134 BTU/lb-°F
@Temperature 400 °C
 0.233 BTU/lb-°F
@Temperature 580.0 °C
Thermal Conductivity 18.0 W/m-K
@Temperature 23.0 °C
 20.2 W/m-K
@Temperature 100 °C
 22.7 W/m-K
@Temperature 200 °C
 24.7 W/m-K
@Temperature 300 °C
 26.1 W/m-K
@Temperature 400 °C
 28.8 W/m-K
@Temperature 500 °C
 35.2 W/m-K
@Temperature 593 °C
 
Processing PropertiesOriginal ValueComments
Processing Temperature 100 °CCritical Temperature Ms
 740 °CCritical Temperature Ac1
 780 °CCritical Temperature Ac2
 
Component Elements PropertiesOriginal ValueComments
Carbon, C 0.21 %
Chromium, Cr 10 %
Cobalt, Co 14 %
Iron, Fe 66.99 %
Molybdenum, Mo 2.0 %
Nickel, Ni 5.5 %
Tungsten, W 1.0 %
Vanadium, V 0.30 %

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
MetalTek MTEK 31 UNS R30031 Cobalt Base Alloy
Titanium Ti-6Al-4V (Grade 5), Annealed
X-40 Cobalt Alloy (UNS R30031)
AISI 4340 Steel, normalized, 25 mm round
Special Metals INCONEL® Alloy 718

NQUEST001 / 121069

Aluminum Castings

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at info@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2025 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.