Aerospace Materials: BERYLLIUM PLATE SR
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 | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| BERYLLIUM PLATE SR 0.251-0.450 S | 70 | 42.5 | 42.5 | 65 | 65 | 45 | 45 | 20 | S | Stress relieved (ground and etched) | 0.067 | 4 | 4 | Plate | 0.1 | AMS 7902 | 0.251-0.450 |
| BERYLLIUM PLATE SR 0.451-0.600 S | 70 | 42.5 | 42.5 | 60 | 60 | 40 | 40 | 20 | S | Stress relieved (ground and etched) | 0.067 | 3 | 3 | Plate | 0.1 | AMS 7902 | 0.451-0.600 |
| BERYLLIUM PLATE SR GE0.601 S | 70 | 42.5 | 42.5 | 40 | 40 | 30 | 30 | 20 | S | Stress relieved (ground and etched) | 0.067 | 1 | 1 | Plate | 0.1 | AMS 7902 | >=0.601 |
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