Aerospace Materials: CH2 AISI 1025 CARBON STEEL TUBING NORMALIZED NA S 2 2 1 0 B C2
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 2 (ksi) | Fcy ksi (ksi) | 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) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AISI 1025 CARBON STEEL TUBING NORMALIZED NA S 2 2 1 0 B C2 | 70 | 29 | 29 | 90 | 36 | 36 | 35 | 55 | 55 | 36 | 36 | 11 | S | Normalized | 0.284 | Tubing | 0.32 | AMS 5075, AMS 5077 ASTM A 108 AMS-T-5066a and | ... |
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