Aerospace Materials: N 155 TUBE 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) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|
| N 155 TUBE ST ANY S | 70 | 29.2 | 29.2 | 100 | 49 | 11.2 | S | Solution treated | 0.3 | Tubing | AMS 5585 |
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