Aerospace Materials: HAYNES HR120 SHEET STRIP PLATE ANN 0.750 TO
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 | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| HAYNES HR120 SHEET STRIP PLATE ANN 0.750 TO 2.000 S | 70 | 90 | 40 | S | Annealed | 0.324 | 30 | Sheet, Strip, and Plate | AMS 5916 | 0.750 to 2.000 |
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