Aerospace Materials: CP-TI SHEET ANN
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 (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CP-TI SHEET ANN 1.000 S T5 2 1 0b C2 | 70 | 15.5 | 16 | 50 | 50 | 40 | 40 | 6.5 | S | Annealed | 0.163 | 20 | 20 | Sheet, strip, and plate | AMS 4902 9046 | 1.000 |
| CP-TI SHEET ANN 1.000 S T5 2 1 0b C3 | 70 | 15.5 | 16 | 65 | 65 | 55 | 55 | 6.5 | S | Annealed | 0.163 | 18 | 18 | Sheet, strip, and plate | AMS 4900 . . AMS-T-9046 and AMS-T-and AMS-T-and AMS-T-and MIL-T-9046 | 1.000 |
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