Aerospace Materials: 2519 PLATE T87
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) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Fcy ksi ST (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) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2519 PLATE T87 ANY S T3 2 11 0b C2 | 70 | 10.5 | 10.8 | 105 | 134 | 85 | 99 | 57 | 60 | — | 41 | 66 | 68 | — | 59 | 58 | — | 4 | S | T87 | 0.102 | 9 | 7 | Plate | 0.33 | MIL-DTL-46192 |
| 2519 PLATE T87 ANY S T3 2 11 0b C3 | 70 | 10.5 | 10.8 | 104 | 133 | 87 | 100 | 58 | 61 | 58 | 41 | 67 | 68 | 63 | 60 | 59 | 55 | 4 | S | T87 | 0.102 | 8 | 6 | Plate | 0.33 | MIL-DTL-46192 |
| 2519 PLATE T87 ANY S T3 2 11 0b C4 | 70 | 10.5 | 10.8 | 103 | 131 | 87 | 100 | 58 | 61 | 58 | 40 | 68 | 68 | 62 | 61 | 59 | 55 | 4 | S | T87 | 0.102 | 7 | 5 | Plate | 0.33 | MIL-DTL-46192 |
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