Aerospace Materials: CUSTOM455 BAR
70 to 1000
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 |
|---|---|---|---|---|---|---|---|---|---|---|
| CUSTOM455 BAR | 70 | 29 | 368 | 227 | 138 | 230 | 220 | 12 | AMS 5578 | up to 3.0 in dia |
| CUSTOM455 BAR | 600 | 28.5 | 312 | 191 | 117 | 195 | 185 | 12 | AMS 5578 | up to 3.0 in dia |
| CUSTOM455 BAR | 800 | 28 | 280 | 169 | 105 | 175 | 163 | 14 | AMS 5578 | up to 3.0 in dia |
| CUSTOM455 BAR | 1,000 | 27 | 208 | 114 | 78 | 130 | 110 | 18 | AMS 5578 | up to 3.0 in dia |
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