Aerospace Materials: CH2 PH13 8MO STAINLESS STEEL NA H950 NA S 2 6 6 0 C C1
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) | Ftu ksi (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi ST (ksi) | RA pct (%) | RA pct ST (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct ST (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 PH13 8MO STAINLESS STEEL NA H950 NA S 2 6 6 0 C C1 | 70 | 28.3 | 220 | 220 | 205 | 205 | 45 | 35 | S | H950 | 0.279 | 10 | 10 | . . . . . . . . . | . . . . . . . . . | . . . . . . . . . |
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