M55J 6k (Toray) carbon fibre (6,000-filament tow) in a 954-3 (Hexcel) cyanate ester matrix, supplied as tape. Carbon/cyanate-ester is chosen for dimensional stability and very low moisture absorption: it outgasses little and resists microcracking through thermal cycling. That makes it a spacecraft-structure and precision-optics material — benches, reflectors, and instrument support — more than an airframe one.
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0/0/0/0/0/0/0/0/0/0/0/0/0/0/0/0]s
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 | |
|---|---|---|---|---|---|
Interlaminar Shear Strength(ILSS) | 76.53 range 68.26–84.12n=113, 6 batches, CV 5.31% | MPa | 22°C · RTA · 13-axis · [0]:32 · as-measured | ||
Ultimate Tensile Strength(σUTS) | 0.7515 – 2.234 | GPa | 8 entriesClick to expand | ||
Young's Modulus(E)4 entries | 328.9 range 300.6–358.5n=109, 6 batches, CV 3.66% | GPa | 22°C · RTA · 1-axis · [0]:16 · norm. thk+FAW | ||
| ↳ | 324.1 range 297.2–359.2n=109, 6 batches, CV 4.21% | GPa | 22°C · RTA · 1-axis · [0]:16 · as-measured | ||
| ↳ | 308.9 range 274.4–339.9n=102, 6 batches, CV 4.7% | GPa | 22°C · RTA · 1-axis · [0]:32 · norm. thk+FAW | ||
| ↳ | 314.4 range 291.6–344.7n=109, 6 batches, CV 3.78% | GPa | 22°C · RTA · 1-axis · [0]:32 · as-measured | ||