Cmh17 Fiber Reference: 2.4.1.7(d)

CMH-17/MIL-HDBK-17-3F fiber and reinforcement reference tables. Includes typical fiber properties (carbon, glass, aramid, boron), nominal composite properties for various reinforcement types, fiber sizing/finish compatibility data, and general reference data from MIL-HDBK-17-3F Chapter 2 and CMH-17 Chapter 6.

Aerospace Engineeringtable_id: 2.4.1.7(d)2 rows
table idrow indexc1c2c3contextsource page
2.4.1.7(d)001PROPERTYRoom Temperature 1/2 hr at 350°F (180°C) U.S. SI U.S. SIMIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties TABLE 2.4.1.7(d) Typical properties for quartz/epoxy. PROPERTY Room Temperature 1/2 hr at 350°F (180°C) U.S.78
2.4.1.7(d)002Tensile Strength (ksi, MPa) Tensile Modulus (Msi, GPa) Flexural Strength (ksi, MPa) Flexural Modulus (Msi, GPa) Compressive Strength (ksi, MPa) Compressive Modulus (Msi, GPa) Laminate Resin Content (wt%) Specific Gravity (g/cm3)74.9 - 104 516 - 717 3.14 - 4.09 21.7 - 28.2 95.5 - 98.9 658 - 682 3.27- 3.46 22.5 - 23.8 66.4 - 72.4 458 - 499 3.43 - 3.75 23.6 - 25.9 33.5 - 32.0 1.73 - 1.7765.4 - 92.2 451 - 636 2.83 - 3.67 19.5 - 25.3 53.9 - 75.9 372 - 523 2.78 - 3.08 19.2 - 21.2 42.6 - 49.9 294 - 344 3.10 - 3.40 21.4 - 23.4MIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties TABLE 2.4.1.7(d) Typical properties for quartz/epoxy. PROPERTY Room Temperature 1/2 hr at 350°F (180°C) U.S.78

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