Aerospace Materials: CH2 PH13 8MO STAINLESS STEEL ROUND HEX SQUARE and FLAT BAR H1000 8 0 A 2 6 6 0 B C3
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) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi ST (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi ST (ksi) | G Msi (Msi) | RA pct (%) | RA pct ST (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct ST (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 PH13 8MO STAINLESS STEEL ROUND HEX SQUARE AND FLAT BAR H1000 8 0 A 2 6 6 0 B C3 | 70 | 28.3 | 29.4 | 302 | 402 | 263 | 338 | 200 | 200 | 117 | 201 | 201 | 190 | 190 | 11 | 50 | 40 | A | H1000 | 0.279 | 10 | 10 | Round, hex, square and flat bar | 0.28 | AMS 5629 | <8.0 |
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