Aerospace Materials: L 605 SHEET ST
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 | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| L 605 SHEET ST 0.010-0.187 A | 70 | 32.6 | 32.6 | 186 | 232 | 88 | 113 | 41 | 56 | 91 | 126 | 130 | 57 | 55 | 12.6 | A | Solution treated | 0.33 | Sheet | 0.29 | AMS 5537 | 0.010-0.187 |
| L 605 SHEET ST 0.010-0.187 B | 70 | 32.6 | 32.6 | 193 | 241 | 96 | 123 | 45 | 61 | 95 | 131 | 135 | 62 | 60 | 12.6 | B | Solution treated | 0.33 | Sheet | 0.29 | AMS 5537 | 0.010-0.187 |
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