Aerospace Materials: CH2 250 MARAGING STEEL SHEET NA 0 187 S 2 5 1 0 B C1
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 250 MARAGING STEEL SHEET NA 0 187 S 2 5 1 0 B C1 | 70 | 28.2 | 247 | S | . | 0.286 | Sheet | 0.31 | . | 0.187 |
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