Aerospace Materials: CH2 9NI 4CO 0 30C STEEL SHEET STRIP and PLATE QUENCHED and TEMPERED 0 249 SB 2 4 3 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 | E Msi (Msi) | Ec Msi (Msi) | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 9NI 4CO 0 30C STEEL SHEET STRIP AND PLATE QUENCHED AND TEMPERED 0 249 SB 2 4 3 0 B C1 | 70 | 28.5 | 29.8 | 220 | 185 | Sb | Quenched and tempered | 0.28 | 6 | Sheet, strip, and plate | AMS 6524a | 0.249 |
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