Rene 41

Applications 

Jet and rocket engines, torque rings, after burners, hardware.

Composition nominal wt. % 

A1 1.6, B 0.007, C 0.06, Co 11.0, Cr 19.0, Fe 3.0, Mo 9.75, Ni rem, Ti 3.15

Specifications 

AMS 5712, 5713.

Density lb/in3 (gcm3) 

0.298 (8.24)

Metallurgical Condition 

1,975°F + age

Tensile Strength ksi (MPa) 

180 (1,241)

0.2% Yield Strength ksi (MPa) 

115 (793)

Elongation % 

20

Reduction in Area % 

25

Hardness 

36 HRC

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