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Aerospace Materials: A 286 STRIP BAR PLATE STA

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: A 286 STRIP BAR PLATE STA5 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fcy ksi LT (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)RA pct (%)RA pct LT (%)RA pct ST (%)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)elongation pct ST (%)formpoisson ratiospecificationthickness range
A 286 STRIP BAR PLATE STA 2.499 S T6 2 1 0b C17029.129.121026614217195911409511.1SSolution treated and aged0.28715strip, Bar plate0.31AMS 5731 5525 AMS 57322.499
A 286 STRIP BAR PLATE STA 2.499 S T6 2 1 0b C27029.129.11952471271538585130130858511.12020SSolution treated and aged0.2871515strip, Bar plate0.31AMS 5731 5525 AMS 57322.499
A 286 STRIP BAR PLATE STA 2.499 S T6 2 1 0b C47029.129.12102661421719591140140959511.11515SSolution treated and aged0.2871212strip, Bar plate0.31AMS 5734 AMS 57372.499
A 286 STRIP BAR PLATE STA 2.500-5.000 S T6 2 1 0b C37029.129.1195247127153858513013013085858511.1202020SSolution treated and aged0.287151515strip, Bar plate0.31AMS 5731 5525 AMS 57322.500-5.000
A 286 STRIP BAR PLATE STA 2.500-5.000 S T6 2 1 0b C57029.129.1210266142171959114014014095959511.1151515SSolution treated and aged0.287121212strip, Bar plate0.31AMS 5734 AMS 57372.500-5.000

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