Cmh17 Fiber Reference: 2.4.1.2(a)
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 | c3 | c4 | c5 | c6 | context | source page |
|---|---|---|---|---|---|---|---|---|---|
| 2.4.1.2(a) | 001 | TABLE 2.4.1.2(a) Nominal composite properties reinforced with aramid fiber (V ~ 60%). f | — | — | — | — | — | MIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties strength (room temperature) of 200 ksi (1.4 GPa) and nominal tensile modulus of 11 Msi (76 GPa). These compo | 61 |
| 2.4.1.2(a) | 002 | — | — | Thermoset (epoxy) | — | Thermoplastic (J2) | — | MIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties strength (room temperature) of 200 ksi (1.4 GPa) and nominal tensile modulus of 11 Msi (76 GPa). These compo | 61 |
| 2.4.1.2(a) | 003 | Tensile Property | Units | unidirectional | fabric1 | unidirectional | fabric1 | MIL-HDBK-17-3F Volume 3, Chapter 2 Materials and Processes - The Effects of Variability on Composite Properties strength (room temperature) of 200 ksi (1.4 GPa) and nominal tensile modulus of 11 Msi (76 GPa). These compo | 61 |
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