Aerospace Materials: INCONEL 706 BAR FORGING HT 2.500-LT2.500
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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| INCONEL 706 BAR FORGING HT 2.500-LT2.500 4.000 S T6 3 4 0b C4 | 70 | 30.4 | 30.4 | 263 | 334 | 195 | 234 | 146 | 106 | 170 | 140 | 11 | 15 | S | Heat treated per indicated specification | 0.292 | 12 | Bar and forging | 0.38 | AMS AMS 5702 and AMS 5701 5606 AMS 5703 | 2.500-<2.500 4.000 |
| INCONEL 706 BAR FORGING HT 2.500-LT2.500 4.000 S T6 3 4 0b C5 | 70 | 30.4 | 30.4 | 263 | 334 | 188 | 226 | 141 | 106 | 170 | 135 | 11 | 15 | S | Heat treated per indicated specification | 0.292 | 12 | Bar and forging | 0.38 | AMS AMS 5702 and AMS 5701 5606 AMS 5703 | 2.500-<2.500 4.000 |
| INCONEL 706 BAR FORGING HT 2.500-LT2.500 4.000 S T6 3 4 0b C6 | 70 | 30.4 | 30.4 | 263 | 334 | 181 | 218 | 136 | 106 | 170 | 130 | 11 | 15 | S | Heat treated per indicated specification | 0.292 | 12 | Bar and forging | 0.38 | AMS AMS 5702 and AMS 5701 5606 AMS 5703 | 2.500-<2.500 4.000 |
| INCONEL 706 BAR FORGING HT 2.500-LT2.500 4.000 S T6 3 4 0b C7 | 70 | 30.4 | 30.4 | 256 | 325 | 181 | 218 | 136 | 103 | 165 | 130 | 11 | 15 | S | Heat treated per indicated specification | 0.292 | 12 | Bar and forging | 0.38 | AMS AMS 5702 and AMS 5701 5606 AMS 5703 | 2.500-<2.500 4.000 |
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