Aerospace Materials: 5052 SHEET UNK
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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 5052 SHEET UNK 0.006-0.128 S | 70 | 10.1 | 10.2 | 62 | 82 | 44 | 51 | — | — | 23 | 39 | 39 | 32 | 32 | 3.85 | S | 0.097 | Sheet | 0.33 | AMS-QQ-A-250/8 | 0.006-0.128 |
| 5052 SHEET UNK 0.006-0.162 S | 70 | 10.1 | 10.2 | 59 | 78 | 41 | 46 | — | — | 22 | 37 | 37 | 29 | 29 | 3.85 | S | 0.097 | Sheet | 0.33 | AMS-QQ-A-250/8 | 0.006-0.162 |
| 5052 SHEET UNK 0.006-3.000 S | 70 | 10.1 | 10.2 | — | — | — | — | — | — | 16 | 25 | — | 9.5 | — | 3.85 | S | 0.097 | Sheet and plate | 0.33 | AMS 4015 | 0.006-3.000 |
| 5052 SHEET UNK 0.009-1.000 S | 70 | 10.1 | 10.2 | 54 | 71 | 37 | 41 | 25 | 26 | 20 | 34 | 34 | 26 | 25 | 3.85 | S | 0.097 | Sheet and plate | 0.33 | AMS 4017 | 0.009-1.000 |
| 5052 SHEET UNK 0.017-2.000 S | 70 | 10.1 | 10.2 | 50 | 65 | 32 | 37 | 22 | 23 | 19 | 31 | 31 | 23 | 22 | 3.85 | S | 0.097 | Sheet and plate | 0.33 | AMS 4016 | 0.017-2.000 |
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