Aerospace Materials: 2219-T87 SHEET
-320 to 70
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) | Fbru ksi (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| 2219-T87 SHEET | -320 | 10.8 | — | 60 | 44 | 75 | 66 | 10 | AMS-QQ-A-250/30 | 0.020-0.499 in |
| 2219-T87 SHEET | 70 | 10.6 | 118 | 52 | 39 | 66 | 57 | 10 | AMS-QQ-A-250/30 | 0.020-0.499 in |
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