AS4/3501-6 Unidirectional Tape (MIL-HDBK-17)
VerifiedcompositeAS4/3501-6 is a unidirectional carbon fiber reinforced epoxy prepreg system combining Hexcel's AS4 carbon fibers (12K tow) with 3501-6 epoxy matrix, designed for autoclave processing at 175°C. This material is a industry-standard choice for aerospace primary structures, defense applications, and high-performance composite parts where fiber alignment in a single direction is critical for load-bearing efficiency. Engineers select it over multi-directional laminates when maximum stiffness and strength along the primary load axis outweigh omnidirectional property needs, and its well-documented MIL-HDBK-17 qualification makes it a preferred baseline for structural certification and damage-tolerance analysis.
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0]T
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Strength(σc) | 41.92 | ksi | T | ||
Poisson's Ratio(ν) | 0.3000 | - | notes | ||
Shear Modulus(G) | 860.1 | ksi | notes | ||
Ultimate Tensile Strength(σUTS) | 8.847 | ksi | T | ||
Young's Modulus(E) | 20,450.3 | ksi | L |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Glass Transition Temperature(Tg) | 391.7 | °F | notes | ||
Thermal Conductivity(k) | 0.3467 | BTU/(hr·ft·°F) | T | ||
Coefficient of Thermal Expansion(α (CTE)) | 13.89 | µin/in·°F | T |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.05708 | lb/in³ | — |