This age hardenable, Iron-Nickel-Chromium alloy is designed for
applications requiring high strength and good corrosion resistance at
temperatures up to 700oC (1290oF).

Applications include:

  • Jet Engines
  • Super Chargers
  • After Burner Parts
  • Fasteners

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Approximate Chemical Composition
Fe 56.5%
Ni 25.5% min
Cr 15%
Ti 2.1% max
Mo 1.25%
DENSITY 7.94 g/cm3 0.287 lb/in3
MELTING POINT 1430oC 2600oF
COEFFICIENT OF EXPANSION 16.4 µm/m °C
( 20 - 100°C)
9.1 x 10-6 in/in °F
( 70 - 212°F)
MODULUS OF RIGIDITY 71.5 kN/m2 10370 ksi
MODULUS OF ELASTICITY 205 kN/m2 29773 ksi
 
CONDITION OF SUPPLY HEAT TREATMENT (AFTER FORMING)
Annealed/Spring Temper Age harden at 705 - 760oC (1300 - 1400oF) for 16 hours and air cool.
 
CONDITION  

APPROX TENSILE STRENGTH

 

APPROX SERVICE TEMPERATURE

Annealed 600-750 N/mm2 87-109 ksi -200o to +400oC -330o to +750oF
Annealed + Aged 1100-1300 N/mm2 159-188 ksi -200o to +400oC -330o to +750oF
Spring Temper 1050-1250 N/mm2 152-181 ksi -200o to +400oC -330o to +750oF
Spring Temper + Aged 1300-1500 N/mm2 188-218 ksi -200o to +400oC -330o to +750oF
 
STANDARDS
AMS 5731 AMS 5734 AMS 5737 AMS 5853 BS HR 650 BS HR 52
 


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