S-2 Glass Roving (Aerospace)

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Key Features

  • Tensile strength ≥4500 MPa — ~30% higher than E-glass
  • Tensile modulus ≥85 GPa — ~15% higher than E-glass
  • Aerospace-qualified glass for rotor spars, missile fairings and armor laminates
  • Epoxy-compatible silane sizing tuned for autoclave and infusion processing
  • Lower cost than carbon fiber with superior impact and fragmentation tolerance

S-2 Glass Roving is a high-strength continuous glass fiber engineered from a magnesium-aluminum-silicate composition, distinct from the calcium-alumino-borosilicate chemistry of standard E-glass. The reformulated glass network delivers single-filament tensile strength ≥4500 MPa — roughly 30% higher than E-glass at 3400 MPa — and tensile modulus ≥85 GPa, about 15% higher than E-glass at 72 GPa. Filament diameter is 9–10 μm and linear density is offered in 1200 tex and 2400 tex options. The sizing is silane-based and tuned for epoxy resin matrices used in aerospace structural composites and ballistic armor laminates.

S-2 glass occupies the niche between standard E-glass and carbon fiber: roughly 4–6× the cost of E-glass but only a fraction of the cost of aerospace carbon, with much better impact and fragmentation behavior than carbon for armor applications. The fiber is the qualified glass reinforcement for helicopter rotor blade D-spars, missile fairings and radomes, lightweight tactical vehicle armor, and high-end sports equipment where the strength-to-cost balance does not justify carbon.

Specifications

ParameterValue
SizingSilane, epoxy-compatible (aerospace-grade)
Density~2.49 g/cm³
Package12–18 kg cylindrical doff, single end
Glass TypeS-2 glass (Mg-Al-silicate, high-strength)
Linear Density1200 tex / 2400 tex (±5%)
Tensile Modulus≥85 GPa
Moisture Content≤0.1%
Filament Diameter9–10 μm
Ignition Loss (LOI)0.4–0.7%
Single-Filament Tensile Strength≥4500 MPa

Applications

Aerospace structural composites (skin and substructure)Helicopter rotor blade D-spar layupMissile fairings, radomes and noseconesLightweight vehicle and crew-compartment armor compositesHigh-end sports equipment (tennis rackets, hockey sticks, sailing masts)

FAQ

Single-filament tensile strength is approximately 4500 MPa for S-2 glass versus 3400 MPa for E-glass — about 30% higher. Tensile modulus is 85 GPa versus 72 GPa — about 15% higher. The cost premium, typically 4–6× E-glass, is only justified when weight matters more than cost: aerospace primary structure, helicopter rotor spars, missile fairings, vehicle and crew armor, and high-end sports equipment. For wind blade root, marine FRP, pultruded structure, FRP pipe and tank — applications where weight is a secondary concern — E-glass or ECR-glass remains the correct choice.

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