Engineered for Multiple Platforms
Fixed Wing UAVs
Optimal aerodynamic integration in internal nacelles or external wings for long endurance flight.
Target Drones
High-G tolerant installation brackets built to withstand pneumatic and rocket launcher catapults.
Ground-Launched Systems
Integration in land-based launchers and cruise systems with rapid startup under 30 seconds.
VTOL / Hybrid UAVs
Vector control integration support for vertical takeoff transitioning to horizontal thrust.
Loitering Munitions
Ultralight, low-profile layouts optimized for high power-to-weight and single-use cost efficiency.
Special Mission Platforms
Engineered solutions tailored to operate in extreme weather, high altitude, or high humidity environments.
Typical Integration Architecture
Our architecture minimizes connection lines down to power supply and a data bus (CAN or RS485). The ECU controls fuel solenoid valves, high-voltage ignition systems, and brushless fuel pumps, separating propulsion loads from flight control hardware.
- • Intelligent Brushless Fuel Pump
- • Fast-Response Fuel Solenoid Valve
- • High-Power Glow Ignition System
- • Integrated Ambient Pressure & Temp Sensors
Flight Control Interfaces
Key Program Benefits
Reduced Integration Time
Streamlines installation via standardized interfaces and plug-and-play config software.
Optimized Performance
Maximizes thrust-to-weight ratio while maintaining low fuel consumption.
Mission Reliability
ECUs and components built and tested to meet critical aerospace and defense standards.
Cost Effective
Minimizes initial developer and tooling costs as well as overall maintenance cycles.
Global Support
On-site and remote engineering support throughout your prototype validation phases.
Explore the propulsion stack