Aerospace Materials: HAYNES 230 PLATE ANN2200 0.401 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 230 PLATE ANN2200 0.401 TO 1.500 A | 70 | 111 | 48 | A | 2200 Anneal | 0.324 | 39 | Plate | AMS 5878 | 0.401 to 1.500 |
| HAYNES 230 PLATE ANN2200 0.401 TO 1.500 B | 70 | 114 | 51 | B | 2200 Anneal | 0.324 | 42 | Plate | AMS 5878 | 0.401 to 1.500 |
What else is in Engineering Database
AI built for engineering. Searches the engineering database, performs calculations, gives source-backed engineering insights.
Get started for free ↗Reference Data375 engineering tablesMaterial properties, pipe and shape dimensions, code tables, and electrical ratings across mechanical, civil, chemical, electrical, materials, and manufacturing engineering.
Browse dataCalculatorsDeterministic engineering calculatorsSizing, checking, and conversion tools that run against the reference tables. Inputs are code-compliant, outputs are traceable to the source standard.
Browse calculators