Chemical Composition
Base Element
C (Carbon)
0.04
%    
Cr (Chromium)
11.5
%    
Fe (Iron)
84.1
%    (estimate)
Ni (Nickel)
4
%    
Ti (Titanium)
0.4
%    
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
619
MPa    
Ultimate Tensile Strength
674
MPa    
Elongation
5
% strain    
 
Other Information
Material Class
Country
USA
Description
Strip Annealed: 123,000 TS; 106,000 YS; 12 El; 28 HRC; At 600 F: 97,700 TS; 89,800 YS; 5 El. For jet engine, missile and space components. Maraging steel, good fracture toughness. Corrosion resistant. Good fabricability.
Designation
ALMAR 363
Specification Type
Specification Status
Source
Available forms
Similar Alloys
 



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