Integrated design, manufacturing, and mission operations spanning atmospheric flight, orbital infrastructure, deep-space exploration, and defense-grade systems engineering.
Scramjet and dual-mode ramjet engines optimized for Mach 5–15 flight regimes. Features adaptive thermal management and AI-driven fuel injection control.
Modular satellite bus platforms with autonomous inter-satellite laser links, drag-compensation thrusters, and on-orbit servicing interfaces.
Wide-body commercial airframes, tactical transport aircraft, and VTOL cargo platforms. Features composite airframes and blended-wing-body aerodynamics.
Nuclear thermal propulsion prototypes, habitat modules, and in-situ resource utilization (ISRU) systems for sustained lunar and cislunar missions.
Unmanned aerial vehicles, drone swarms, electronic warfare suites, and real-time battlefield intelligence processing pipelines.
Vertical and horizontal launch pads, fueling systems, range safety networks, and rapid-recovery booster landing zones across 6 global sites.
Full-flow staged combustion cycle engines delivering 2.1 MN thrust. Designed for high-thrust orbital insertion and reusable first-stage recovery.
Hall-effect and gridded ion thrusters for station-keeping, debris removal, and deep-space cargo transfer. >8,000s specific impulse.
Automated cleanroom assembly, radiation-hardened processors, and deployable solar arrays rated for 15+ year LEO service.
Additively manufactured wing spars, active flow control surfaces, and fly-by-wire flight computers with triple-redundant AI oversight.
Multi-role combat air vehicles, directed-energy weapon mounts, and encrypted datalink networks meeting MIL-STD-810H and ITAR compliance.
| System | Thrust / Power | Max Velocity | Operating Ceiling | Reliability / MTBF |
|---|---|---|---|---|
| AZ-HV7 Scramjet | 185 kN (sea level) | Mach 7.5 | 32,000 m | 4,200 hrs |
| Zenth-Orbital Bus v4 | 12 kW Solar Array | N/A (LEO) | 200–2,000 km | 12,000 hrs |
| AZ-99 Main Stage Engine | 2.1 MN (vac) | Orbital Injection | Vacuum | 8,500 hrs |
| Sentinel-X MALE UAV | Dual GE F414 | Mach 0.85 | 14,500 m | 6,000 hrs |
| Lunar Ascent Vehicle | 320 kN (NTP) | 2.5 km/s Δv | Cislunar | 1,800 hrs |
Our aerospace engineering team provides NDA-covered white papers, CAD integration kits, and custom mission architecture consultations.