Aerospace Materials: 2014 FORGING T652
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 (%) | elongation pct ST (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2014 FORGING T652 7.001-8.000 S | 70 | 10.5 | 10.8 | — | — | — | — | — | — | — | — | 59 | 59 | 57 | 51 | 51 | 48 | 4 | S | T652b | 0.101 | 6 | 2 | 1 | Hand forging | 0.33 | AMS-A-22771 and AMS-QQ-A-367 | 7.001-8.000 |
| 2014 FORGING T652 LE1.000 A | 70 | 10.5 | 10.8 | 91 | 123 | 73 | 90 | 56 | — | 59 | 40 | 65 | — | — | 56 | — | — | 4 | A | T652 | 0.101 | 6 | — | — | Die forging | 0.33 | AMS-A-22771 and AMS-QQ-A-367 | <=1.000 |
| 2014 FORGING T652 LE1.000 B | 70 | 10.5 | 10.8 | 94 | 127 | 77 | 94 | 59 | — | 62 | 41 | 67 | — | — | 59 | — | — | 4 | B | T652 | 0.101 | — | — | — | Die forging | 0.33 | AMS-A-22771 and AMS-QQ-A-367 | <=1.000 |
| 2014 FORGING T652 LE2.000 S | 70 | 10.5 | 10.8 | 88 | 115 | 77 | 91 | 56 | 57 | — | 38 | 65 | 65 | — | 56 | 56 | — | 4 | S | T652b | 0.101 | 8 | 3 | — | Hand forging | 0.33 | AMS-A-22771 and AMS-QQ-A-367 | <=2.000 |
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