Chemical Composition
Base Element
C (Carbon)
0.05
%  (maximum)  
Cr (Chromium)
14 to 14.5
%    
Fe (Iron)
69.5 to 79.2
%    (estimate)
Ni (Nickel)
6.25 to 7
%    
Ti (Titanium)
0.6 to 9
%    
Balance
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.
 
Mechanical Properties
Yield Strength
745
MPa    
Ultimate Tensile Strength
862
MPa    
Elongation
16
% strain    
Rockwell Hardness C scale
25
   
 
Other Information
Material Class
Country
USA
Description
Annealed: 125,000 TS; 108,000 YS; 16 El; 25 HRC; Age Hardened: 188,000 TS; 182,000 YS; 13 El, 41 HRC; For jet engine, aircraft and missile components, hydraulic and pneumatic equipment, valve and pump parts.
Designation
ALMAR 362
Specification Type
Specification Status
Similar UNS Number
S36200
Source
Available forms
Similar Alloys
 



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