|
Applications:
Airframe structurals, missile components, valve parts, fasteners, chemical process equipment.
Composition, nominal wt. %
C 0.035, Cb 0.3, Cr 14.5, Cu 3.5, Mn 0.5, Ni 4.75, P 0.02, S 0.015, Si 0.5
Specifications
AMS 5659. ASTM A 564/564 M, A 705/705 M.
|
| 13-8 MO |
| Density lb/in3 (g/cm3) |
0.279 (7.72) |
| Metallurgical Condition |
1,700°F + age |
| Tensile Strength, ksi (MPa) |
215 (1,483) |
| 0.2% Yield Strength, ksi (MPa) |
200 (1,379) |
| Elongation, % |
10 |
| Reduction in Area, % |
40 |
| Typical Hardness |
44 HRC | |
