CFRP T700/2510 Unidirectional
VerifiedcompositeCFRP T700/2510 is a unidirectional carbon fiber reinforced polymer composite combining Toray's T700S carbon fibers with a 2510 epoxy matrix, processed as an out-of-autoclave (OOA) prepreg system that cures at moderate temperature without requiring autoclave equipment. This material is widely used in aerospace, defense, and performance-critical structures where weight savings, stiffness, and damage tolerance are essential—particularly in secondary structures, control surfaces, and components where the out-of-autoclave processing reduces manufacturing cost and facility overhead compared to autoclave-dependent systems. The unidirectional fiber orientation makes it ideal for applications requiring directional strength optimization, and the 2510 epoxy matrix offers good toughness and environmental resistance, making it a practical choice for engineers balancing performance demands with manufacturing simplicity.
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 | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 1.700 | - | — | ||
Poisson's Ratio(ν) | 0.3000 | - | — | ||
Ultimate Tensile Strength(σUTS) | 304.6 | ksi | — | ||
Young's Modulus(E) | 19,145 | ksi | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Maximum Service Temperature(Tmax) | 249.5 | °F | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.05636 | lb/in³ | — |