Read the following passage:
During composite component fabrication for aircraft frames, carbon-fiber prepreg layers are cured under elevated heat and pressure inside an industrial autoclave. High hydrostatic pressure compresses the resin matrix into the structural fibers while forcing entrapped volatile gases and air voids into vacuum collection bags before thermal cross-linking solidifies the matrix. If pressure drops prematurely during the exothermic heating phase, internal resin boiling creates micro-voids that significantly reduce structural shear strength. However, maintaining maximum pressure beyond the resin gel point provides no structural benefit and increases operating energy costs.
Match each statement about the composite curing process to its correct logical status based strictly on the passage evidence.
- Premature pressure loss during exothermic heating reduces composite shear strength due to internal void development.Supported inference derived directly from textual evidence linking pressure retention, void prevention, and shear strength.
- Continuing peak autoclave pressure past the resin gel point improves the component's final structural properties.Contradicted claim directly refuted by passage evidence indicating that post-gel pressure provides zero structural gain.
- Industrial autoclaves are the only manufacturing systems capable of curing carbon-fiber aircraft components.Unsupported assumption introducing an unwarranted exclusivity claim regarding manufacturing equipment.
- The primary role of hydrostatic pressure in the autoclave is to accelerate the exothermic cross-linking reaction.Unsupported causal distortion that misidentifies mechanical compression and void extraction as thermal acceleration.