6. Typical tensile strength is 530,000
psi. Matrix: 934 is a high flow, epoxy resin with good hot/wet properties and meets NASA outgassing requirements. Maximum Short Term Service Temperature: 350°F (dry), 200°F (wet) Typical applications: Aircraft primary and secondary structure, critical space structure.
Fiber: T-300 fibers are continuous, no twist carbon filaments made from PAN precursor, surface
treated to improve handling characteristics and structural properties. Filament count is
3,000 filamentshow. Typical tensile modulus is 33 X 1 06. Typical tensile strength is 530,000