Aerospace Materials: CP-TI BAR 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) | Fbru ksi (ksi) | Fbry ksi (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | G Msi (Msi) | RA pct (%) | RA pct LT (%) | RA pct ST (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | elongation pct ST (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CP-TI BAR ANN 2.999 S T5 2 1 0b C4 | 70 | 15.5 | 16 | 120 | 101 | 70 | 70 | 42 | 80 | 80 | — | 70 | 70 | — | 6.5 | — | — | — | S | Annealed | 0.163 | 15 | 15 | — | Bar | AMS 4901 9046 | 2.999b |
| CP-TI BAR ANN 2.999 S T5 2 1 0b C5 | 70 | 15.5 | 16 | — | — | — | — | — | 80 | 80 | — | 70 | 70 | — | 6.5 | 30 | 30 | — | S | Annealed | 0.163 | 15 | 15 | — | Bar | AMS 4921 MIL-T-9047a 9047 | 2.999b |
| CP-TI BAR ANN 3.000-4.000 S | 70 | 15.5 | 16 | — | — | — | — | — | 80 | 80 | 80 | 70 | 70 | 70 | 6.5 | 30 | 30 | 30 | S | Annealed | 0.163 | 15 | 15 | 15 | Bar | AMS 4921 MIL-T-9047a 9047 | 3.000-4.000b |
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