Range attributes
C (Carbon)
0.12
%    
Cr (Chromium)
4
%    
Fe (Iron)
86.9
%    (estimate)
Mo (Molybdenum)
4.25
%    
Ni (Nickel)
3.5
%    
Rockwell Hardness C scale
58 to 62
   
V (Vanadium)
1.2
%    
 
Logical attributes
Bearing
Yes
 
Discrete attributes
~Checking Status
Available forms
Balance
Base Element
Country
USA
Material Class
Source
Specification Status
Specification Type
 
Short text attributes
Composition Note_old
Fe is listed as a Balance element for this material, but its % value is not listed in the specification. The value shown is a calculated one.
Country*
USA
Description_old
Surface hardness of 58-62 HRC obtained by carburizing. Modified M-50 high temperature bearing steel developed by G.E. Aircraft Engine Div. as M50 NiL. Capable of high fracture toughness and rolling contact fatigue life.
Designation
AL TECH HTB-5
 
Long text attributes
Composition Note
Fe is listed as a Balance element for this material, but its % value is not listed in the specification. The value shown is a calculated one.
Description
Surface hardness of 58-62 HRC obtained by carburizing. Modified M-50 high temperature bearing steel developed by G.E. Aircraft Engine Div. as M50 NiL. Capable of high fracture toughness and rolling contact fatigue life.
 
Hyperlink attributes
Similar Alloys
 
Integer attributes
ID
60515
Source ID
231893
 
Further Information
 



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