Aerospace Materials: CH2 280 MARAGING STEEL PLATE MARAGED AT 900 F 0 188 0 250 S 2 5 1 0 C C2
Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).
| material id | temp f | Ec Msi (Msi) | Ftu ksi (ksi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| CH2 280 MARAGING STEEL PLATE MARAGED AT 900 F 0 188 0 250 S 2 5 1 0 C C2 | 70 | 28.6 | 276 | S | Maraged at 900(F | 0.286 | Plate | 0.31 | AMS 6521a | 0.188-0.250 |
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