A Nickel-Chromium-Cobalt alloy being precipitation hardenable, having
high stress-rupture strength and creep resistance at high temperatures
up to about 950OC (1740OF). It is widely used and a well proven alloy in high temperature conditions.

Applications include:

  • Aerospace Industry
  • High Temperature Springs and Various
  • Thermal Processing

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Approximate Chemical Composition
Ni 54% min
Cr 18-21%
Co 15-21%
Ti 2-3%
Al 1-2%
DENSITY   8.18 g/cm3 0.296 lb/in3
MELTING POINT   1370oC 2500oF
COEFFICIENT OF EXPANSION   12.7 µm/m °C
( 20 - 100°C)
7.1 x 10-6 in/in °F
( 70 - 212°F)
MODULUS OF RIGIDITY   82.5 kN/mm2 11966 ksi
MODULUS OF ELASTICITY *
**
213 kN/m2
227 / 240 kN/mm2
30894 ksi
32924 / 34810 ksi
* Solution Annealed + Aged **Spring Temper and Aged
CONDITION OF SUPPLY HEAT TREATMENT (AFTER FORMING)
Solution Annealed Age harden at 750oC (1380oF) for 4 hours and air cool. *
Spring Temper Age harden at 650oC (1200oF) for 4 hours and air cool. *
Spring Temper Age harden at 600oC (1110oF) for 16 hours and air cool. *
 
CONDITION  

APPROX TENSILE STRENGTH

 

APPROX SERVICE TEMPERATURE

Solution Annealed 800-1000 N/mm2 116-145 ksi - -
Solution Annealed + Aged 1300-1400 N/mm2 189-203 ksi up to 550oC up to 1020oF
Spring Temper 1300-1500 N/mm2 189-218 ksi - -
Spring Temper + Aged 1500-1800 N/mm2 218-261 ksi up to 350oC up to 660oF
 
STANDARDS
BS HR 501
(Spring temper)
BS HR 502
(Solution Annealed)
BS HR 503 BS 3075 NA19 AMS 5829 NCK20TA
 


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