Aerospace Materials: CH2 5CR MO V AIRCRAFT STEEL SHEET STRIP and PLATE NA NA NA SA 2 4 1 0 D 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 | E Msi (Msi) | Ec Msi (Msi) | Fbru ksi 2 (ksi) | Fbry ksi 2 (ksi) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 5CR MO V AIRCRAFT STEEL SHEET STRIP AND PLATE NA NA NA SA 2 4 1 0 D C1 | 70 | 30 | 30 | 400 | 315 | 220 | 144 | 240 | 200 | 11 | Sa | . . . . . . . | 0.281 | . . . . . . . | 0.36 | . . . . . . . | . . . . . . . |
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