L-605

 

Applications 

High temperature applications, jet engine components, devices in high fatigue service.

Composition nominal wt. % 

C 0.1, Co rem, Cr 20.0, Fe 0.5, Mn 1.7, Ni 10.0, W 15.0

Specifications 

AMS 5759, 5844.
ASTM F 90; B50T26

Density lb/in3 (gcm3) 

0.333 (9.22)

Metallurgical Condition 

2,200°F anneal

Tensile Strength ksi (MPa) 

150 (1,035)

0.2% Yield Strength ksi (MPa) 

60 (414)

Elongation % 

60

Reduction in Area % 

40

Hardness 

80 HRB

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