Solid Rocket Motor Propulsion
Segmented solid rocket motor architectures engineered for heavy orbital ascent, tactical stage separation, and rapid missile booster ignition under sub-zero theater conditions.
Automated Composite Aerostructures
Continuous fiber placement producing carbon-epoxy payload shrouds, interstage barrels, and hypersonic wing control surfaces with high structural rigidity and minimal mass.
Precision Strike Architecture
Hardened munition casings, tactical warhead integration, and precision guidance housing designed to penetrate reinforced subterranean defenses with sub-millimeter tolerances.
High-Stress Mechanical Assemblies
High-Altitude Tactical Separation
Pneumatic and pyrotechnic payload release mechanisms qualified for high-Mach multi-stage jettison sequences without structural deflection.
Thermal Protection Barriers
Elastomeric ablative coatings and ceramic tile matrices guarding structural alloys against intense aerodynamic friction during hypersonic atmospheric transit.
Large-Diameter Composite Cases
Autoclave-cured carbon-phenolic solid rocket cases withstanding internal combustion chamber pressures exceeding 2,500 psi across sustained burn durations.
Environmental Qualification Thresholds
3,200 °F
plume flame threshold
48 g
tri-axial vibrational load
180 s
continuous static burn
100%
ultrasonic joint inspection
Direct delivery of payload interface specifications and CAD models for cleared defense contractors and program managers.