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Aerospace Materials: 7475-T761 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: 7475-T761 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
7475-T761 ARAMID ARAMID LAM ANY 0.032 S709.87.79.67.89196108104737684834651241035676482.82.6S0.0851.56.1Aramid fiber reinforced sheet laminate2/10.350.25AMS 43020.032
7475-T761 ARAMID ARAMID LAM ANY 0.053 S709.97.19.67.383858887706976814648231115182432.62.4S0.0831.86.4Aramid fiber reinforced sheet laminate3/20.350.25AMS 43020.053
7475-T761 ARAMID ARAMID LAM ANY 0.074 S70106.79.6784868688666975774447221145082422.32.3S0.0821.76.3Aramid fiber reinforced sheet laminate4/30.350.25AMS 43020.074
7475-T761 ARAMID ARAMID LAM ANY 0.094 S709.86.79.76.982808084696772794445211164884402.32.3S0.0811.86.6Aramid fiber reinforced sheet laminate5/40.350.25AMS 43020.094

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