Applications
Jet engines, superchargers, missile components, fasteners, cryogenic equipment, nuclear, corrosive deep well hardware.
Composition nominal wt. % Al 0.18, B 0.006, C 0.04, Cr 14.8, Mn 1.0, Mo 1.3, Ni 25.5, P 0.02, S 0.015, Si 0.5, Ti 2.13, V 0.3
Specifications AMS 5525, 5731, 5732, 5734, 5737.
MIL-S-24550; ASTM A 453.
Density lb/in3 (gcm3) MIL-S-24550; ASTM A 453.
0.286 (7.92)
Metallurgical Condition
1,800°F + age
Tensile Strength ksi (MPa) 150 (1,035)
0.2% Yield Strength ksi (MPa) 110 (759)
Elongation % 25
Reduction in Area % 40
Hardness 32 HRC
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