Flight-critical composite structures

150 PSI

autoclave consolidation pressure

0.05 mm

machined envelope tolerance

450°F

continuous thermal rating

100%

ultrasound NDT verification

Oriented along load vectors

Every ply is positioned in an ISO Class 7 cleanroom under strict humidity and temperature controls. Technicians index prepreg unidirectional carbon fibers along computed stress paths to maximize tensile modulus while reducing unnecessary mass.

Laser projection alignment systems verify ply placement within tenths of a millimeter before vacuum debulking, eliminating internal voids and bridging across complex structural compound curves.

Integrated composite manufacturing

From initial tooling design to final ultrasonic non-destructive verification, our facility executes every flight-critical process under traceable aerospace quality standards.

Invar Tooling & Analysis

High-Pressure Autoclaves

Ultrasonic NDT Scanning

Finite element laminate optimization paired with low-expansion invar and carbon composite tooling to eliminate thermal warpage during cure cycles.

Computer-controlled cure cycles up to 150 PSI with inert nitrogen atmospheres prevent laminate porosity and guarantee matrix density.

Phased-array ultrasonic testing rigs and multi-axis coordinate measuring machines verify internal bonding integrity and dimensional accuracy.

Provide 3D CAD geometry, target ply schedules, or performance envelopes. Our structural engineers deliver preliminary feasibility analyses and tooling estimates under mutual non-disclosure agreements.