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Aerospace Materials: 2024-T3 ARAMID ARAMID LAM

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: 2024-T3 ARAMID ARAMID LAM4 rows
material idtemp fE Msi (Msi)E Msi LTEc Msi (Msi)Ec Msi LTFbru ksi LFbru ksi LTFbru ksi LT 2Fbru ksi L 2Fbry ksi LFbry ksi LTFbry ksi LT 2Fbry ksi L 2Fcy 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)G Msi LTbasisdensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)formlaminate layuppoisson ratiopoisson ratio LTspecificationthickness range
2024-T3 ARAMID ARAMID LAM ANY 0.032 S709.98.19.587889959353566663353316904848332.72.6S0.086212Aramid fiber reinforced sheet laminate2/10.330.29AMS 42540.032
2024-T3 ARAMID ARAMID LAM ANY 0.053 S709.97.59.47.57384898652526163353015964449302.52.4S0.084212Aramid fiber reinforced sheet laminate3/20.340.27AMS 42540.053
2024-T3 ARAMID ARAMID LAM ANY 0.074 S709.77.19.37.273808183515261613430141014349302.42.4S0.082212Aramid fiber reinforced sheet laminate4/30.340.26AMS 42540.074
2024-T3 ARAMID ARAMID LAM ANY 0.094 S709.679.1768757677505260593330141014249302.22.2S0.081214Aramid fiber reinforced sheet laminate5/40.320.25AMS 42540.094

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