Aerospace Materials: HS 188 SHEET 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) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | 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 LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| HS 188 SHEET ST 0.020-0.187 S | 70 | 33.6 | 33.6 | 55 | 111 | 125 | 125 | 57 | 55 | 12.8 | S | Solution Treated | 0.324 | 45 | Sheet | 0.31 | AMS 5608 | 0.020-0.187 |
| HS 188 SHEET ST LT0.020 S | 70 | 33.6 | 33.6 | 55 | 111 | 125 | 125 | 57 | 55 | 12.8 | S | Solution Treated | 0.324 | 40 | Sheet | 0.31 | AMS 5608 | <0.020 |
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