Aerospace Materials: BERYLLIUM BAR ROD TUBE HP
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) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| BERYLLIUM BAR ROD TUBE HP ANY S | 70 | 42 | 42 | 47 | 47 | 35 | 35 | 20 | S | Hot pressed (ground and etched) | 0.067 | 2 | 2 | Bar, rod, tubing, and machined shapes | 0.1 | AMS 7906 |
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