Sample data from Engineering Database — 375 reference tables, deterministic calculators, and Engineering AI. Sign up free

Aerospace Materials: A286 BAR

70 to 1500

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).

Materials Sciencematerial id: A286 BAR10 rows
material idtemp fE Msi (Msi)Fbru ksi (ksi)Fcy ksi (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Fty ksi (ksi)elongation pct (%)specificationthickness range
A286 BAR7029.124785851308515AMS 5731 (AMS 5732)≤2.499 in dia
A286 BAR40014393.521.5AMS 5731 (1800°F ST + 1325°F/16h aged)bar
A286 BAR80014195AMS 5731 / AMS 5734 (test heat treatment: 1650°F/2h OQ + 1300°F/16h AC)bar (0.250 in dia specimen)
A286 BAR1,000137101AMS 5731 / AMS 5734 (test heat treatment: 1650°F/2h OQ + 1300°F/16h AC)bar (0.250 in dia specimen)
A286 BAR1,10022.81229021AMS 5731 (1800°F ST + 1325°F/16h aged)bar
A286 BAR1,20021.9103.58813AMS 5731 (1800°F ST + 1325°F/16h aged)bar
A286 BAR1,25011097AMS 5731 / AMS 5734 (test heat treatment: 1650°F/2h OQ + 1300°F/16h AC)bar (0.250 in dia specimen)
A286 BAR1,30021.186.58611AMS 5731 (1800°F ST + 1325°F/16h aged)bar
A286 BAR1,40020.1646218.5AMS 5731 (1800°F ST + 1325°F/16h aged)bar
A286 BAR1,50018.736.53368.5AMS 5731 (1800°F ST + 1325°F/16h aged)bar

What else is in Engineering Database

Related data