Cmh17 Fiber Reference: 2.4.1.4
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.
| table id | row index | c1 | c2 | context | source page |
|---|---|---|---|---|---|
| 2.4.1.4 | 001 | — | Value, ksi (MPa) | MIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties Available almost exclusively in filament or epoxy matrix prepreg form, boron fiber has been used for aerospa | 71 |
| 2.4.1.4 | 002 | Moduli Tensile, longitudinal Tensile, transverse Strength Tensile, longitudinal Tensile, transverse Compressive, longitudinal | 30 (207) 2.7 (19) 192 (1323) 10.4 (72) 353 (2432) | MIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties Available almost exclusively in filament or epoxy matrix prepreg form, boron fiber has been used for aerospa | 71 |
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